1.5 m trisonic wind tunnel

The 1.5 m trisonic wind tunnel has played an instrumental part of Canadian and international research and development into the aerodynamics of aircraft and defence systems. This facility has a demonstrated track record in performing aerodynamic assessment through a wide range of operational envelopes over subsonic through to high supersonic flow conditions. These test capabilities have been developed in a secure environment to deliver high-quality aerodynamic data of complete test articles and their sub components.

Follow the NRC LinkedIn Twitter Instagram Web feeds

What we offer

The 1.5 m trisonic wind tunnel is a pressurized, intermittent-flow wind tunnel capable of providing subsonic, transonic and supersonic flows, Mach 0.1 to 4.25. Independent control of the stagnation pressure over the full operational envelope permits a range of Reynolds numbers to be simulated while maintaining a constant Mach number.

A high-mass flow compressor plant maintains high test productivity. Time to recharge between runs is less than 30 minutes.

The facility offers three main test configurations to meet a number of test requirements.

Why work with us

The NRC has recognized expertise in wind tunnel correction methodologies, pressure-sensitive paint technology, model deformation measurement capability and flow mapping. Our world-renowned team includes aerodynamicists, flight engineers and business experts that will support your research initiatives with professional services and industry know-how. Working in our unique facilities to test, validate and demonstrate your product provides a controlled environment to de-risk new and experimental products with reliable data that will be critical in the large-scale or commercial development of your product.

We also have prominent competencies in:

  • aeroacoustic measurement, testing and evaluation, which can determine three-dimensional sound fields generated by a model in a wind tunnel
  • flight vehicle aerodynamics
  • ground vehicle and ground-based structures aerodynamics
  • icing formation, detection and mitigation, including a significant capability to experimentally and numerically study the effects of icing on the performance of fixed-wing aircraft, helicopters and cables
  • sports aerodynamics, preparing athletes with critical data that can maximize speed and performance

Technical specification

Test arrangements

The facility offers three main test arrangements to meet a number of different requirements:

3D test

This standard test arrangement permits the model to be mounted from a downstream strut with a roll drive, sting and internal balance. Automated pitch-roll combinations within the limits of -14 to +28°, and ±360°, respectively, permit a wide range of model angles of attack and sideslip to be obtained.

For the subsonic and transonic regimes, the model is tested in the transonic test section. This test section makes use of perforated wall boundaries enclosed in a pressure-tight plenum and is easily installed in the circuit downstream of the supersonic nozzle using automated systems. Control of the Mach number is achieved using a servo controlled diffuser throat area or plenum outflow flaps with fixed nozzle geometries. The Mach number is infinitely variable up to Mach 1.2.

For supersonic testing (typically Mach 1.4 and above), the transonic test section is taken out of line and the test region is at the end of the supersonic nozzle. The supersonic nozzle has a 2D flexible wall with 16 nozzle geometries providing 16 discrete Mach numbers covering Mach 1 to Mach 4.25. A single blow-down can provide between 30 to 40 seconds of runtime for all Mach numbers below Mach 4 with unit Reynolds numbers in the range of 15 to 20 million/m. Higher Reynolds numbers (up to 80 million/m) will result in lower available run times.

A production mode system is also available to perform stores release studies. The parent model is mounted from a separate sting off of the ceiling of the transonic test section. The store under study is supported on its own balance and is traversed over an array of prescribed vectors from its carriage position. These data provide the aerodynamic coefficients of the store within the flow field of the releasing aircraft.

A blade/plate mount is also available for subsonic-transonic conditions.

Typical uses of this test arrangement include stores clearance for military aircraft, weapon aerodynamics research, and stability and control of aircraft in cruise and high lift configurations.

Half-model

For these tests, a solid reflection plane is mounted off a wall of the standard 3D transonic test section. The starboard (or inverted port) half of the aircraft is built as a model and mounted to an external six component balance. The model is typically pitched at a rate of 2° to 3° per second during the run. The pitch range is ±50° but is constrained in practice by the model length. This mode of testing permits a model of approximately double the scale of the standard 3D arrangement, providing higher Reynolds number, improved access for surface pressure tap instrumentation, and an ability to accurately represent flaps, slats, and other component features.

Subsonic and transonic conditions are available for this arrangement. With a typically sized aircraft model, Reynolds numbers based on the mean aerodynamic chord of over 23 million/m can be achieved from Mach 0.2 to Mach 1, with 12 or more seconds of usable run time.

Typical uses of this test arrangement include stability and control of aircraft in cruise and high lift configurations and contaminated wing tests (e.g., ice accretions).

2D test

Through the use of the roll-in roll-out interchangeable transonic test section system, the 3D transonic test section can be replaced with a 1.5 m high by 0.38 m wide transonic channel. This test section is suitable for testing airfoil profiles or other section shapes over the Mach range of 0.1 to 1.0. Chord Reynolds numbers of 130 to 160 million/m can be achieved with typical model chord lengths at Mach numbers above 0.6.

Typical uses of this test arrangement include rotary wing airfoil development, evaluation of active flow control concepts, civil engineering studies of bluff body sections at high Reynolds number and wind turbine blade designs.

Measurement techniques

  • Internal and external strain-gauge balances for force and moment measurements
  • Digitally scanned pressure transducers for extensive discrete surface pressure measurements
  • Surface flow visualization using fluorescent mini tufts imaged at approximately 5 frames per second where each image is annotated with synchronized model measurements
  • Multi-focused Schlieren off surface flow visualization in the 3-D supersonic and transonic modes
  • Pressure-sensitive paint (PSP) to optically measure pressures over entire model surfaces
  • Non-intrusive optical model deformation measurement capability to assess the wind-on deflected twist and displacement of wings or other highly loaded flexible components
  • Optical tracking of models while being moved with load-deflected supports (a standard technique for stores release testing)
  • Model deformation measurements using stereography imaging

Performance charts and run tables

Figure A - Subsonic performance Mach 0.1 - Mach 0.7.
Figure A. Long description follows.

Performance Data for Mach 0.100

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 0.125 0.0085 8.417x105 2.761x106 282.1
20.0 1.361 0.139 0.0095 9.352x105 3.068x106 250.4
22.0 1.498 0.153 0.0104 1.029x106 3.375x106 224.6
24.0 1.634 0.167 0.0114 1.122x106 3.682x106 203.0
26.0 1.770 0.181 0.0123 1.216x106 3.989x106 184.9
28.0 1.906 0.195 0.0132 1.309x106 4.295x106 139.3
30.0 2.042 0.209 0.0142 1.403x106 4.602x106 155.8
32.0 2.178 0.222 0.0151 1.496x106 4.909x106 144.1
34.0 2.314 0.236 0.0161 1.590x106 5.216x106 133.8
36.0 2.451 0.250 0.0170 1.683x106 5.523x106 124.6
38.0 2.587 0.264 0.0180 1.777x106 5.830x106 116.4
40.0 2.723 0.278 0.0189 1.870x106 6.136x106 109.0
42.0 2.859 0.292 0.0199 1.964x106 6.443x106 102.3
44.0 2.995 0.306 0.0208 2.057x106 6.750x106 96.3
46.0 3.131 0.320 0.0218 2.151x106 7.057x106 90.8
48.0 2.268 0.334 0.0227 2.244x106 7.364x106 85.7
50.0 3.404 0.348 0.0237 2.338x106 7.671x106 81.1
55.0 3.744 0.382 0.0260 2.572x106 8.438x106 71.0
60.0 4.084 0.417 0.0284 2.806x106 9.205x106 62.6
65.0 4.425 0.452 0.0308 3.039x106 9.972x106 55.5
70.0 4.765 0.487 0.0331 3.273x106 1.074x107 49.4
75.0 5.106 0.521 0.0355 3.507x106 1.151x107 44.2
80.0 5.446 0.556 0.0379 3.741x106 1.227x107 39.6
85.0 5.786 0.591 0.0402 3.975x106 1.304x107 35.5
90.0 6.127 0.626 0.0426 4.208x106 1.381x107 31.9
95.0 6.467 0.660 0.0450 4.442x106 1.457x107 28.7
100.0 6.807 0.695 0.0473 4.676x106 1.534x107 25.8
105.0 7.148 0.730 0.0497 4.910x106 1.611x107 23.1
110.0 7.488 0.765 0.0521 5.144x106 1.688x107 20.6
115.0 7.828 0.799 0.0544 5.377x106 1.794x107 18.4
120.0 8.169 0.834 0.0568 5.611x106 1.841x107 16.2
125.0 8.509 0.869 0.0591 5.845x106 1.918x107 14.2
130.0 8.850 0.904 0.0615 6.079x106 1.994x107 12.3

Performance Data for Mach 0.150

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 0.279 0.0190 1.256x106 4.119x106 187.6
20.0 1.361 0.310 0.0211 1.395x106 4.577x106 166.4
22.0 1.498 0.341 0.0232 1.535x106 5.035x106 149.1
24.0 1.634 0.372 0.0253 1.674x106 5.492x106 134.7
26.0 1.770 0.403 0.0274 1.814x106 5.950x106 122.4
28.0 1.906 0.434 0.0296 1.953x106 6.408x106 112.0
30.0 2.042 0.465 0.0317 2.093x106 6.865x106 103.1
32.0 2.178 0.496 0.0338 2.323x106 7.323x106 95.2
34.0 2.314 0.527 0.0359 2.372x106 7.781x106 88.3
36.0 2.451 0.558 0.0380 2.511x106 8.238x106 82.1
38.0 2.587 0.589 0.0401 2.651x106 8.696x106 76.6
40.0 2.723 0.620 0.0422 2.790x106 9.154x106 71.7
42.0 2.859 0.651 0.0443 2.930x106 9.611x106 67.2
44.0 2.995 0.682 0.0464 3.069x106 1.007x107 63.1
46.0 3.131 0.713 0.0486 3.209x106 1.053x107 59.4
48.0 2.268 0.744 0.0507 3.348x106 1.098x107 56.0
50.0 3.404 0.775 0.0528 3.488x106 1.144x107 52.9
55.0 3.744 0.853 0.0580 3.836x106 1.259x107 46.2
60.0 4.084 0.930 0.0633 4.185x106 1.373x107 40.6
65.0 4.425 1.008 0.0686 4.534x106 1.487x107 35.8
70.0 4.765 1.085 0.0739 4.883x106 1.602x107 31.8
75.0 5.106 1.163 0.0792 5.231x106 1.716x107 28.2
80.0 5.446 1.240 0.0844 5.580x106 1.831x107 25.2
85.0 5.786 1.318 0.0897 5.929x106 1.945x107 22.4
90.0 6.127 1.395 0.0950 6.278x106 2.060x107 20.0
95.0 6.467 1.473 0.1003 6.626x106 2.174x107 17.8
100.0 6.807 1.550 0.1055 6.975x106 2.288x107 15.8
105.0 7.148 1.628 0.1108 7.324x106 2.403x107 14.0
110.0 7.488 1.705 0.1161 7.673x106 2.517x107 12.4
115.0 7.828 1.783 0.1214 8.021x106 2.632x107 10.8
120.0 8.169 1.861 0.1267 8.370x106 2.746x107 9.3
125.0 8.509 1.938 0.1319 8.719x106 2.861x107 7.9
130.0 8.850 2.016 0.1372 9.068x106 2.975x107 6.5
135.0 9.190 2.093 0.1425 9.416x106 3.089x107 4.9

Performance Data for Mach 0.200

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 0.490 0.0334 1.661x106 5.450x106 140.7
20.0 1.361 0.545 0.0371 1.846x106 6.055x106 124.7
22.0 1.498 0.599 0.0408 2.030x106 6.661x106 111.6
24.0 1.634 0.654 0.0445 2.215x106 7.266x106 100.6
26.0 1.770 0.708 0.0482 2.399x106 7.872x106 91.5
28.0 1.906 0.762 0.0519 2.584x106 8.478x106 83.6
30.0 2.042 0.817 0.0556 2.769x106 9.083x106 76.9
32.0 2.178 0.871 0.0593 2.953x106 9.689x106 70.8
34.0 2.314 0.926 0.0630 3.138x106 1.029x107 65.5
36.0 2.451 0.980 0.0667 3.322x106 1.090x107 60.9
38.0 2.587 1.035 0.0704 3.507x106 1.151x107 56.8
40.0 2.723 1.089 0.0741 3.691x106 1.211x107 53.0
42.0 2.859 1.144 0.0779 3.876x106 1.272x107 49.6
44.0 2.995 1.198 0.0816 4.061x106 1.332x107 46.6
46.0 3.131 1.253 0.0853 4.245x106 1.393x107 43.8
48.0 2.268 1.307 0.0890 4.430x106 1.453x107 41.2
50.0 3.404 1.361 0.0927 4.614x106 1.514x107 38.9
55.0 3.744 1.498 0.1020 5.076x106 1.665x107 33.8
60.0 4.084 1.634 0.1112 5.537x106 1.817x107 29.5
65.0 4.425 1.770 0.1205 5.998x106 1.968x107 26.0
70.0 4.765 1.906 0.1298 6.460x106 2.119x107 22.9
75.0 5.106 2.042 0.1390 6.921x106 2.271x107 20.2
80.0 5.446 2.178 0.1483 7.383x106 2.422x107 17.9
85.0 5.786 2.315 0.1576 7.844x106 2.574x107 15.8
90.0 6.127 2.451 0.1668 8.306x106 2.725x107 14.0
95.0 6.467 2.587 0.1761 8.767x106 2.876x107 12.3
100.0 6.807 2.723 0.1854 9.228x106 3.028x107 10.8
105.0 7.148 2.859 0.1946 9.690x106 3.179x107 9.4
110.0 7.488 2.995 0.2039 1.015x107 3.330x107 8.1
115.0 7.828 3.131 0.2132 1.061x107 3.482x107 6.9
120.0 8.169 3.268 0.2224 1.107x107 3.633x107 5.7
125.0 8.509 3.404 0.2317 1.154x107 3.785x107 4.5
130.0 8.850 3.540 0.2410 1.200x107 3.936x107 3.1

Performance Data for Mach 0.250

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 0.754 0.0513 2.056x106 6.745x106 112.8
20.0 1.361 0.838 0.0570 2.284x106 7.495x106 99.9
22.0 1.498 0.922 0.0627 2.513x106 8.244x106 90.2
24.0 1.634 1.005 0.0684 2.741x106 8.993x106 80.4
26.0 1.770 1.089 0.0741 2.970x106 9.743x106 73.0
28.0 1.906 1.173 0.0798 3.198x106 1.049x107 66.8
30.0 2.042 1.257 0.0855 3.427x106 1.124x107 61.1
32.0 2.178 1.340 0.0912 3.655x106 1.199x107 56.2
34.0 2.314 1.424 0.0970 3.883x106 1.274x107 52.0
36.0 2.451 1.508 0.1027 4.112x106 1.349x107 48.2
38.0 2.587 1.592 0.1084 4.340x106 1.424x107 44.9
40.0 2.723 1.676 0.1141 4.569x106 1.499x107 41.9
42.0 2.859 1.759 0.1198 4.797x106 1.574x107 39.1
44.0 2.995 1.843 0.1255 5.026x106 1.649x107 36.6
46.0 3.131 1.927 0.1312 5.254x106 1.742x107 34.4
48.0 2.268 2.011 0.1369 5.482x106 1.799x107 32.4
50.0 3.404 2.094 0.1426 5.711x106 1.874x107 30.4
55.0 3.744 2.304 0.1568 6.282x106 2.061x107 26.3
60.0 4.084 2.513 0.1711 6.853x106 2.248x107 22.9
65.0 4.425 2.723 0.1853 7.424x106 2.436x107 20.0
70.0 4.765 2.932 0.1996 7.955x106 2.623x107 17.5
75.0 5.106 3.142 0.2139 8.566x106 2.810x107 15.3
80.0 5.446 3.351 0.2281 9.137x106 2.998x107 13.4
85.0 5.786 3.561 0.2424 9.708x106 3.185x107 11.7
90.0 6.127 3.770 0.2566 1.028x107 3.373x107 10.2
95.0 6.467 3.997 0.2709 1.085x107 3.560x107 8.9
100.0 6.807 4.189 0.2852 1.142x107 3.747x107 7.7
105.0 7.148 4.398 0.2994 1.199x107 3.935x107 6.5
110.0 7.488 4.608 0.3137 1.256x107 4.122x107 5.4
115.0 7.828 4.817 0.3279 1.313x107 4.309x107 4.4
120.0 8.169 5.027 0.3422 1.371x107 4.497x107 3.3

Performance Data for Mach 0.300

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 1.065 0.0725 2.438x106 7.997x106 94.4
20.0 1.361 1.184 0.0806 2.708x106 8.886x106 83.5
22.0 1.498 1.302 0.0886 2.979x106 9.774x106 74.5
24.0 1.634 1.420 0.0967 3.250x106 1.066x107 67.0
26.0 1.770 1.539 0.1048 3.521x106 1.155x107 60.7
28.0 1.906 1.657 0.1128 3.792x106 1.244x107 55.3
30.0 2.042 1.776 0.1209 4.063x106 1.333x107 50.6
32.0 2.178 1.894 0.1289 4.333x106 1.422x107 46.6
34.0 2.314 2.012 0.1370 4.604x106 1.511x107 43.0
36.0 2.451 2.131 0.1450 4.875x106 1.599x107 39.8
38.0 2.587 2.249 0.1531 5.146x106 1.688x107 37.0
40.0 2.723 2.367 0.1612 5.417x106 1.777x107 34.4
42.0 2.859 2.486 0.1692 5.688x106 1.866x107 32.2
44.0 2.995 2.604 0.1773 5.958x106 1.955x107 30.1
46.0 3.131 2.723 0.1853 6.229x106 2.044x107 28.1
48.0 2.268 2.841 0.1934 6.500x106 2.133x107 26.4
50.0 3.404 2.959 0.2015 6.771x106 2.221x107 24.8
55.0 3.744 3.255 0.2216 7.448x106 2.444x107 21.3
60.0 4.084 3.551 0.2417 8.125x106 2.666x107 18.4
65.0 4.425 3.847 0.2619 8.802x106 2.888x107 16.0
70.0 4.765 4.143 0.2820 9.479x106 3.110x107 13.9
75.0 5.106 4.439 0.3022 1.016x107 3.332x107 12.0
80.0 5.446 4.735 0.3223 1.083x107 3.554x107 10.4
85.0 5.786 5.031 0.3425 1.151x107 3.776x107 9.0
90.0 6.127 5.327 0.3626 1.219x107 3.999x107 7.7
95.0 6.467 5.623 0.3828 1.286x107 4.221x107 6.5
100.0 6.807 5.919 0.4029 1.354x107 4.443x107 5.5
105.0 7.148 6.215 0.4230 1.422x107 4.665x107 4.5
110.0 7.488 6.511 0.4432 1.490x107 4.887x107 3.5
115.0 7.828 6.806 0.4633 1.557x107 5.109x107 2.4

Performance Data for Mach 0.350

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 1.418 0.0965 2.804x106 9.199x106 81.5
20.0 1.361 1.576 0.1073 3.115x106 1.022x107 71.9
22.0 1.498 1.733 0.1180 3.427x106 1.124x107 64.0
24.0 1.634 1.891 0.1287 3.738x106 1.227x107 57.6
26.0 1.770 2.048 0.1394 4.050x106 1.329x107 52.1
28.0 1.906 2.206 0.1502 4.362x106 1.431x107 47.4
30.0 2.042 2.364 0.1609 4.673x106 1.533x107 43.3
32.0 2.178 2.521 0.1716 4.985x106 1.635x107 39.8
34.0 2.314 2.679 0.1823 5.296x106 1.738x107 36.7
36.0 2.451 2.836 0.1931 5.608x106 1.840x107 33.9
38.0 2.587 2.994 0.2038 5.919x106 1.942x107 31.4
40.0 2.723 3.151 0.2145 6.231x106 2.044x107 29.2
42.0 2.859 3.309 0.2253 6.542x106 2.146x107 27.2
44.0 2.995 3.467 0.2360 6.854x106 2.249x107 25.4
46.0 3.131 3.624 0.2467 7.165x106 2.351x107 23.7
48.0 2.268 3.782 0.2574 7.477x106 2.453x107 22.2
50.0 3.404 3.939 0.2682 7.788x106 2.555x107 20.8
55.0 3.744 4.333 0.2950 8.567x106 2.811x107 17.8
60.0 4.084 4.727 0.3218 9.346x106 3.066x107 16.2
65.0 4.425 5.121 0.3486 1.012x107 6.322x107 13.1
70.0 4.765 5.515 0.3754 1.090x107 3.577x107 11.3
75.0 5.106 5.909 0.4022 1.168x107 3.833x107 9.7
80.0 5.446 6.303 0.4291 1.246x107 4.088x107 8.3
85.0 5.786 6.697 0.4559 1.324x107 4.344x107 7.0
90.0 6.127 7.091 0.4827 1.402x107 4.599x107 5.9
95.0 6.467 7.485 0.5095 1.480x107 4.855x107 4.8
100.0 6.807 7.878 0.5363 1.558x107 5.111x107 3.9
105.0 7.148 8.272 0.5631 1.636x107 5.366x107 2.9

Performance Data for Mach 0.400

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 1.806 0.1229 3.153x106 1.034x107 71.9
20.0 1.361 2.006 0.1366 3.503x106 1.149x107 63.5
22.0 1.498 2.207 0.1502 3.854x106 1.264x107 56.5
24.0 1.634 2.407 0.1639 4.204x106 1.379x107 50.7
26.0 1.770 2.608 0.1775 4.554x106 1.494x107 45.8
28.0 1.906 2.809 0.1912 4.904x106 1.609x107 41.5
30.0 2.042 3.009 0.2049 5.255x106 1.724x107 37.9
32.0 2.178 3.210 0.2185 5.605x106 1.839x107 34.8
34.0 2.314 3.410 0.2322 5.955x106 1.954x107 32.0
36.0 2.451 3.611 0.2458 6.306x106 2.069x107 29.5
38.0 2.587 3.812 0.2595 6.656x106 2.184x107 27.3
40.0 2.723 4.012 0.2731 7.006x106 2.299x107 25.3
42.0 2.859 1.213 0.2868 7.357x106 2.414x107 23.6
44.0 2.995 4.414 0.3004 7.707x106 2.529x107 21.9
46.0 3.131 4.614 0.3141 8.057x106 2.643x107 20.5
48.0 2.268 4.815 0.3278 8.408x106 2.758x107 19.1
50.0 3.404 5.015 0.3414 8.758x106 2.873x107 17.8
55.0 3.744 5.517 0.3756 9.634x106 3.161x107 15.1
60.0 4.084 6.019 0.4097 1.051x107 3.448x107 12.9
65.0 4.425 6.520 0.4438 1.139x107 3.735x107 11.0
70.0 4.765 7.022 0.4780 1.226x107 4.023x107 9.3
75.0 5.106 7.523 0.5121 1.314x107 4.310x107 7.9
80.0 5.446 8.025 0.5463 1.401x107 4.597x107 6.6
85.0 5.786 8.526 0.5804 1.489x107 4.885x107 5.5
90.0 6.127 9.028 0.6146 1.576x107 5.172x107 4.5
95.0 6.467 9.529 0.6487 1.664x107 5.459x107 3.5
100.0 6.807 10.031 0.6828 1.752x107 5.747x107 2.5

Performance Data for Mach 0.450

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 2.220 0.1512 3.483x106 1.143x107 64.8
20.0 1.361 2.467 0.1680 3.870x106 1.270x107 57.0
22.0 1.498 2.714 0.1847 4.257x106 1.397x107 50.7
24.0 1.634 2.961 0.2015 4.644x106 1.524x107 45.4
26.0 1.770 3.207 0.2183 5.031x106 1.651x107 41.0
28.0 1.906 3.454 0.2351 5.418x106 1.778x107 37.2
30.0 2.042 3.701 0.2519 5.805x106 1.905x107 33.8
32.0 2.178 3.948 0.2687 6.192x106 2.031x107 31.0
34.0 2.314 4.194 0.2855 6.579x106 2.158x107 28.4
36.0 2.451 4.441 0.3023 6.966x106 2.285x107 26.2
38.0 2.587 4.688 0.3191 7.353x106 2.412x107 24.2
40.0 2.723 4.934 0.3359 7.740x106 2.539x107 22.4
42.0 2.859 5.181 0.3527 8.127x106 2.666x107 20.8
44.0 2.995 5.428 0.3695 8.514x106 2.793x107 19.3
46.0 3.131 5.675 0.3863 8.901x106 2.920x107 17.9
48.0 2.268 5.921 0.4031 9.288x106 3.047x107 16.7
50.0 3.404 6.168 0.4199 9.675x106 3.174x107 15.6
55.0 3.744 6.785 0.4619 1.064x107 3.492x107 13.1
60.0 4.084 7.402 0.5039 1.161x107 3.809x107 11.1
65.0 4.425 8.018 0.5458 1.258x107 4.126x107 9.3
70.0 4.765 8.635 0.5878 1.354x107 4.444x107 7.8
75.0 5.106 9.252 0.6298 1.451x107 4.761x107 6.5
80.0 5.446 9.869 0.6718 1.548x107 5.079x107 5.3
85.0 5.786 10.486 0.7138 1.645x107 5.396x107 4.3
90.0 6.127 11.102 0.7558 1.741x107 5.714x107 3.3
95.0 6.467 11.719 0.7978 1.838x107 6.031x107 2.3

Performance Data for Mach 0.500

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 2.656 0.1808 3.793x106 1.244x107 59.2
20.0 1.361 2.951 0.2009 4.214x106 1.383x107 52.0
22.0 1.498 3.246 0.2209 4.636x106 1.521x107 46.2
24.0 1.634 3.541 0.2410 5.057x106 1.659x107 41.3
26.0 1.770 3.836 0.2611 5.478x106 1.797x107 37.2
28.0 1.906 4.131 0.2812 5.900x106 1.936x107 33.7
30.0 2.042 4.426 0.3013 6.321x106 2.074x107 30.7
32.0 2.178 4.721 0.3214 6.743x106 2.212x107 28.0
34.0 2.314 5.016 0.3415 7.164x106 2.350x107 25.7
36.0 2.451 5.311 0.3615 7.585x106 2.489x107 23.6
38.0 2.587 5.606 0.3816 8.007x106 2.627x107 21.8
40.0 2.723 5.901 0.4017 8.428x106 2.765x107 20.1
42.0 2.859 6.196 0.4218 8.850x106 2.903x107 18.6
44.0 2.995 6.491 0.4419 8.271x106 3.042x107 17.3
46.0 3.131 6.786 0.4620 9.693x106 3.180x107 16.0
48.0 2.268 7.081 0.4821 1.011x107 3.318x107 14.9
50.0 3.404 7.376 0.5021 1.054x107 3.456x107 13.8
55.0 3.744 8.114 0.5524 1.159x107 3.802x107 11.6
60.0 4.084 8.852 0.6026 1.264x107 4.148x107 9.7
65.0 4.425 9.589 0.6528 1.370x107 4.493x107 8.0
70.0 4.765 10.327 0.7030 1.475x107 4.839x107 6.6
75.0 5.106 11.065 0.7532 1.580x107 5.185x107 5.4
80.0 5.446 11.802 0.8034 1.686x107 5.530x107 4.3
85.0 5.786 12.540 0.8536 1.791x107 5.876x107 3.3
90.0 6.127 13.278 0.9039 1.896x107 6.222x107 2.2

Performance Data for Mach 0.550

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 3.103 0.2122 4.081x106 1.339x107 54.9
20.0 1.361 3.448 0.2347 4.534x106 1.488x107 48.2
22.0 1.498 3.793 0.2582 4.988x106 1.636x107 42.7
24.0 1.634 4.138 0.2817 5.441x106 1.785x107 38.2
26.0 1.770 4.482 0.3051 5.895x106 1.934x107 34.3
28.0 1.906 4.827 0.3286 6.348x106 2.083x107 31.0
30.0 2.042 5.172 0.3521 6.802x106 2.232x107 28.2
32.0 2.178 5.517 0.3755 7.255x106 2.380x107 25.7
34.0 2.314 5.862 0.3990 7.709x106 2.529x107 23.5
36.0 2.451 6.206 0.4225 8.162x106 2.678x107 21.6
38.0 2.587 6.551 0.4460 8.615x106 2.827x107 19.9
40.0 2.723 6.896 0.4694 9.069x106 2.975x107 18.3
42.0 2.859 7.241 0.4929 9.522x106 3.124x107 16.9
44.0 2.995 7.586 0.5164 9.976x106 3.273x107 15.6
46.0 3.131 7.930 0.5398 1.043x107 3.422x107 14.5
48.0 2.268 8.275 0.5633 1.088x107 3.570x107 13.4
50.0 3.404 8.620 0.5868 1.134x107 3.719x107 12.4
55.0 3.744 9.482 0.6455 1.247x107 4.091x107 10.3
60.0 4.084 10.344 0.7042 1.360x107 4.463x107 8.5
65.0 4.425 11.206 0.7628 1.474x107 4.835x107 7.0
70.0 4.765 12.068 0.8215 1.587x107 5.207x107 5.7
75.0 5.106 12.930 0.8802 1.700x107 5.579x107 4.5
80.0 5.446 13.792 0.9389 1.814x107 5.951x107 3.4
85.0 5.786 14.654 0.9975 1.927x107 6.323x107 2.2

Performance Data for Mach 0.600

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 3.556 0.2421 4.347x106 1.426x107 51.5
20.0 1.361 3.951 0.2690 4.830x106 1.585x107 45.1
22.0 1.498 4.347 0.2959 5.313x106 1.743x107 40.0
24.0 1.634 4.742 0.3228 5.796x106 1.902x107 35.6
26.0 1.770 5.137 0.3497 6.279x106 2.060x107 32.0
28.0 1.906 5.532 0.3766 6.762x106 2.218x107 28.9
30.0 2.042 5.927 0.4035 7.245x106 2.377x107 26.2
32.0 2.178 6.322 0.4304 7.728x106 2.535x107 23.9
34.0 2.314 6.717 0.4573 8.211x106 2.694x107 21.8
36.0 2.451 7.112 0.4842 8.694x106 2.852x107 20.0
38.0 2.587 7.508 0.5111 9.177x106 3.011x107 18.3
40.0 2.723 7.903 0.5380 9.660x106 3.169x107 16.9
42.0 2.859 8.298 0.5649 1.014x107 3.328x107 15.6
44.0 2.995 8.693 0.5918 1.063x107 3.486x107 14.4
46.0 3.131 9.088 0.6187 1.111x107 3.645x107 13.3
48.0 2.268 9.483 0.6456 1.159x107 3.803x107 12.2
50.0 3.404 9.878 0.6725 1.207x107 3.962x107 11.3
55.0 3.744 10.866 0.7397 1.328x107 4.358x107 9.3
60.0 4.084 11.854 0.8070 1.449x107 4.754x107 7.6
65.0 4.425 12.842 0.8742 1.570x107 5.150x107 6.1
70.0 4.765 13.830 0.9414 1.690x107 5.546x107 4.8
75.0 5.106 14.818 1.0087 1.811x107 5.942x107 3.6

Performance Data for Mach 0.650

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 4.008 0.2728 4.590x106 1.506x107 48.8
20.0 1.361 4.453 0.3061 5.100x106 1.673x107 42.7
22.0 1.498 4.898 0.3334 5.610x106 1.841x107 37.8
24.0 1.634 5.344 0.3638 6.120x106 2.008x107 33.7
26.0 1.770 5.789 0.3941 6.630x106 2.175x107 30.2
28.0 1.906 6.234 0.4244 7.140x106 2.342x107 27.2
30.0 2.042 6.679 0.4547 7.650x106 2.510x107 24.7
32.0 2.178 7.125 0.4850 8.160x106 2.677x107 22.5
34.0 2.314 7.570 0.5153 8.670x106 2.844x107 20.5
36.0 2.451 8.015 0.5456 9.180x106 3.012x107 18.7
38.0 2.587 8.461 0.5759 9.690x106 3.179x107 17.2
40.0 2.723 8.906 0.6063 1.020x107 3.346x107 15.8
42.0 2.859 9.351 0.6366 1.071x107 3.514x107 14.5
44.0 2.995 9.797 0.6669 1.122x107 3.681x107 13.4
46.0 3.131 10.242 0.6972 1.173x107 3.848x107 12.3
48.0 2.268 10.687 0.7275 1.224x107 4.016x107 11.4
50.0 3.404 11.132 0.7578 1.275x107 4.183x107 10.5
55.0 3.744 12.246 0.8336 1.402x107 4.601x107 8.5
60.0 4.084 13.359 0.9094 1.530x107 5.020x107 6.9
65.0 4.425 14.472 0.9852 1.657x107 5.438x107 5.5
70.0 4.765 15.585 1.0610 1.785x107 5.856x107 4.3
75.0 5.106 16.699 1.1367 1.912x107 6.274x107 3.1

Performance Data for Mach 0.700

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 4.451 0.3030 4.810x106 1.578x107 43.0
20.0 1.361 4.946 0.3367 5.344x106 1.753x107 37.6
22.0 1.498 5.440 0.3703 5.878x106 1.929x107 33.1
24.0 1.634 5.935 0.4040 6.413x106 2.104x107 29.4
26.0 1.770 6.429 0.4377 6.947x106 2.279x107 26.3
28.0 1.906 6.924 0.4713 7.482x106 2.455x107 23.7
30.0 2.042 7.418 0.5050 8.016x106 2.630x107 21.4
32.0 2.178 7.913 0.5387 8.551x106 2.805x107 19.4
34.0 2.314 8.407 0.5723 9.085x106 2.981x107 17.6
36.0 2.451 8.902 0.6060 9.619x106 3.156x107 16.0
38.0 2.587 9.397 0.6397 1.015x107 3.331x107 14.7
40.0 2.723 9.891 0.6733 1.069x107 3.507x107 13.4
42.0 2.859 10.386 0.7070 1.122x107 3.682x107 12.2
44.0 2.995 10.880 0.7407 1.176x107 3.857x107 11.2
46.0 3.131 11.375 0.7743 1.229x107 4.033x107 10.3
48.0 2.268 11.869 0.8080 1.283x107 4.208x107 9.4
50.0 3.404 12.364 0.8417 1.336x107 4.383x107 8.6
55.0 3.744 13.600 0.9258 1.470x107 4.822x107 6.9
60.0 4.084 14.837 1.0100 1.603x107 5.260x107 5.4
65.0 4.425 16.073 1.0942 1.737x107 5.698x107 4.2
70.0 4.765 17.309 1.1783 1.870x107 3.137x107 3.0
75.0 5.106 18.546 1.2625 2.004x107 6.575x107 2.0
Figure B - Transonic performance Mach 0.7 - Mach 1.4.
Figure B. Long description follows.

Performance Data for Mach 0.750

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 4.880 0.3322 5.006x106 1.642x107 43.0
20.0 1.361 5.423 0.3691 5.562x106 1.825x107 37.6
22.0 1.498 5.965 0.4060 6.119x106 2.007x107 33.1
24.0 1.634 6.507 0.4430 6.675x106 2.190x107 29.4
26.0 1.770 7.049 0.4799 7.231x106 2.372x107 26.3
28.0 1.906 7.592 0.5168 7.787x106 2.555x107 23.7
30.0 2.042 8.134 0.5537 8.344x106 2.737x107 21.4
32.0 2.178 8.676 0.5906 8.900x106 2.920x107 19.4
34.0 2.314 9.218 0.6275 9.456x106 3.102x107 17.6
36.0 2.451 9.761 0.6644 1.001x107 3.285x107 16.0
38.0 2.587 10.303 0.7013 1.057x107 3.467x107 14.7
40.0 2.723 10.845 0.7383 1.112x107 3.650x107 13.4
42.0 2.859 11.387 0.7752 1.168x107 3.832x107 12.2
44.0 2.995 11.930 0.8121 1.224x107 4.015x107 11.2
46.0 3.131 12.472 0.8490 1.279x107 4.197x107 10.3
48.0 2.268 13.014 0.8859 1.335x107 4.380x107 9.4
50.0 3.404 13.556 0.9228 1.391x107 4.562x107 8.6
55.0 3.744 14.912 1.0151 1.530x107 5.019x107 6.9
60.0 4.084 16.268 1.1074 1.669x107 5.475x107 5.4
65.0 4.425 17.623 1.1997 1.808x107 5.931x107 4.2
70.0 4.765 18.979 1.2920 1.947x107 6.387x107 3.0
75.0 5.106 20.334 1.3842 2.086x107 6.843x107 2.0

Performance Data for Mach 0.800

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 5.290 0.3601 5.179x106 1.699x107 43.0
20.0 1.361 5.878 0.4001 5.755x106 1.888x107 37.6
22.0 1.498 6.466 0.4401 6.330x106 2.077x107 33.1
24.0 1.634 7.045 0.4802 6.906x106 2.266x107 29.4
26.0 1.770 7.641 0.5202 7.481x106 2.455x107 26.3
28.0 1.906 8.229 0.5602 8.057x106 2.643x107 23.7
30.0 2.042 8.817 0.6002 8.632x106 2.832x107 21.4
32.0 2.178 9.405 0.66402 9.208x106 3.021x107 19.4
34.0 2.314 9.993 0.6802 9.783x106 3.210x107 17.6
36.0 2.451 10.580 0.7202 1.036x107 3.399x107 16.0
38.0 2.587 11.168 0.7603 1.093x107 3.587x107 14.7
40.0 2.723 11.756 0.8003 1.151x107 3.776x107 13.4
42.0 2.859 12.344 0.8403 1.209x107 3.965x107 12.2
44.0 2.995 12.932 0.8803 1.266x107 4.154x107 11.2
46.0 3.131 13.519 0.9203 1.324x107 4.343x107 10.3
48.0 2.268 14.107 0.9603 1.381x107 4.531x107 9.4
50.0 3.404 14.695 1.0003 1.439x107 4.720x107 8.6
55.0 3.744 16.164 1.1004 1.583x107 5.192x107 6.9
60.0 4.084 17.634 1.2004 1.726x107 5.664x107 5.4
65.0 4.425 19.103 1.3004 1.870x107 6.136x107 4.2
70.0 4.765 20.573 1.4005 2.014x107 6.608x107 3.0
75.0 5.106 22.042 1.5005 2.158x107 7.080x107 2.0

Performance Data for Mach 0.850

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 5.676 0.3864 5.330x106 1.749x107 43.0
20.0 1.361 6.307 0.4293 5.922x106 1.943x107 37.6
22.0 1.498 6.938 0.4732 6.515x106 2.137x107 33.1
24.0 1.634 7.568 0.5151 7.107x106 2.332x107 29.4
26.0 1.770 8.199 0.5581 7.699x106 2.526x107 26.3
28.0 1.906 8.830 0.6011 8.291x106 2.270x107 23.7
30.0 2.042 9.460 0.6440 8.883x106 2.915x107 21.4
32.0 2.178 10.091 0.6869 9.476x106 3.109x107 19.4
34.0 2.314 10.722 0.7299 1.007x107 3.303x107 17.6
36.0 2.451 11.352 0.7728 1.066x107 3.497x107 16.0
38.0 2.587 11.983 0.8157 1.125x107 3.692x107 14.7
40.0 2.723 12.614 0.8587 1.184x107 3.886x107 13.4
42.0 2.859 13.244 0.9016 1.244x107 4.080x107 12.2
44.0 2.995 13.875 0.9445 1.303x107 4.275x107 11.2
46.0 3.131 14.506 0.9875 1.362x107 4.469x107 10.3
48.0 2.268 15.136 1.0304 1.421x107 4.663x107 9.4
50.0 3.404 15.767 1.0733 1.481x107 4.858x107 8.6
55.0 3.744 17.344 1.1806 1.629x107 5.343x107 6.9
60.0 4.084 18.920 1.2880 1.777x107 5.829x107 5.4
65.0 4.425 20.497 1.3953 1.925x107 6.315x107 4.2
70.0 4.765 22.074 1.5026 2.073x107 6.801x107 3.0
75.0 5.106 23.651 1.6100 2.221x107 7.286x107 2.0

Performance Data for Mach 0.900

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 6.034 0.4108 5.458x106 1.791x107 43.0
20.0 1.361 6.705 0.4564 6.065x106 1.990x107 37.6
22.0 1.498 7.375 0.5021 6.671x106 2.189x107 33.1
24.0 1.634 8.046 0.5477 7.278x106 2.388x107 29.4
26.0 1.770 8.716 0.5934 7.884x106 2.587x107 26.3
28.0 1.906 9.387 0.6390 8.481x106 2.786x107 23.7
30.0 2.042 10.057 0.6846 9.097x106 2.985x107 21.4
32.0 2.178 10.728 0.7303 9.704x106 3.184x107 19.4
34.0 2.314 11.398 0.7759 1.031x107 3.383x107 17.6
36.0 2.451 12.069 0.8216 1.092x107 3.582x107 16.0
38.0 2.587 12.739 0.8672 1.152x107 3.781x107 14.7
40.0 2.723 13.410 0.9129 1.213x107 3.980x107 13.4
42.0 2.859 14.080 0.9585 1.274x107 4.179x107 12.2
44.0 2.995 14.751 1.0041 1.334x107 4.378x107 11.2
46.0 3.131 15.421 1.0498 1.395x107 4.577x107 10.3
48.0 2.268 16.092 1.0954 1.456x107 4.776x107 9.4
50.0 3.404 16.762 1.1411 1.516x107 4.975x107 8.6
55.0 3.744 18.438 1.2552 1.668x107 5.472x107 6.9
60.0 4.084 20.115 1.3693 1.819x107 5.969x107 5.4
65.0 4.425 21.791 1.4834 1.971x107 6.467x107 4.2
70.0 4.765 23.467 1.5975 2.123x107 6.964x107 3.0
75.0 5.106 25.143 1.7116 2.274x107 7.462x107 2.0

Performance Data for Mach 0.950

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 6.362 0.4331 5.565x106 1.826x107 43.0
20.0 1.361 7.062 0.4812 6.184x106 2.029x107 37.6
22.0 1.498 7.776 0.5293 6.802x106 2.232x107 33.1
24.0 1.634 8.483 0.5774 7.420x106 2.435x107 29.4
26.0 1.770 9.189 0.6256 8.039x106 2.637x107 26.3
28.0 1.906 9.896 0.6737 8.657x106 2.840x107 23.7
30.0 2.042 10.603 0.7218 9.276x106 3.043x107 21.4
32.0 2.178 11.310 0.7699 9.894x106 3.246x107 19.4
34.0 2.314 12.017 0.8180 1.051x107 3.449x107 17.6
36.0 2.451 12.724 0.8662 1.113x107 3.652x107 16.0
38.0 2.587 13.431 0.9143 1.175x107 3.855x107 14.7
40.0 2.723 14.138 0.9624 1.237x107 4.058x107 13.4
42.0 2.859 14.844 1.0105 1.299x107 4.260x107 12.2
44.0 2.995 15.551 1.0586 1.360x107 4.463x107 11.2
46.0 3.131 16.258 1.1068 1.422x107 4.666x107 10.3
48.0 2.268 16.965 1.1549 1.484x107 4.869x107 9.4
50.0 3.404 17.672 1.2030 1.546x107 5.072x107 8.6
55.0 3.744 19.439 1.3233 1.701x107 5.579x107 6.9
60.0 4.084 21.206 1.4436 1.855x107 6.086x107 5.4
65.0 4.425 22.974 1.5639 2.010x107 6.594x107 4.2
70.0 4.765 24.741 1.6842 2.164x107 7.101x107 3.0
75.0 5.106 26.508 1.8045 2.319x107 7.608x107 2.0

Performance Data for Mach 1.000

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 6.656 0.4531 5.652x106 1.854x107 43.0
20.0 1.361 7.396 0.5035 6.280x106 2.060x107 37.6
22.0 1.498 8.136 0.5538 6.908x106 2.266x107 33.1
24.0 1.634 8.875 0.6042 7.536x106 2.472x107 29.4
26.0 1.770 9.615 0.6545 8.163x106 2.678x107 26.3
28.0 1.906 10.354 0.7049 8.791x106 2.884x107 23.7
30.0 2.042 11.094 0.7552 9.419x106 3.090x107 21.4
32.0 2.178 11.834 0.8055 1.005x107 3.296x107 19.4
34.0 2.314 12.573 0.8559 1.068x107 3.502x107 17.6
36.0 2.451 13.313 0.9062 1.130x107 3.708x107 16.0
38.0 2.587 14.052 0.9566 1.193x107 3.914x107 14.7
40.0 2.723 14.792 1.0069 1.256x107 4.120x107 13.4
42.0 2.859 15.531 1.0573 1.319x107 4.326x107 12.2
44.0 2.995 16.271 1.1079 1.382x107 4.533x107 11.2
46.0 3.131 17.011 1.1580 1.444x107 4.739x107 10.3
48.0 2.268 17.750 1.2083 1.504x107 4.945x107 9.4
50.0 3.404 18.490 1.2587 1.570x107 5.151x107 8.6
55.0 3.744 20.339 1.3845 1.727x107 5.666x107 6.9
60.0 4.084 22.188 1.5104 1.884x107 6.181x107 5.4
65.0 4.425 24.037 1.6363 2.041x107 6.696x107 4.2
70.0 4.765 25.886 1.7621 2.198x107 7.211x107 3.0
75.0 5.106 27.735 1.8880 2.355x107 7.726x107 2.0

Performance Data for Mach 1.050

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 6.916 0.4708 5.718x106 1.876x107 41.6
20.0 1.361 7.685 0.5231 6.354x106 2.085x107 36.3
22.0 1.498 8.453 0.5754 6.989x106 2.293x107 32.0
24.0 1.634 9.222 0.6277 7.624x106 2.501x107 28.4
26.0 1.770 9.990 0.6801 8.260x106 2.710x107 25.4
28.0 1.906 10.759 0.7324 8.895x106 2.918x107 22.8
30.0 2.042 11.527 0.7847 9.531x106 3.127x107 20.6
32.0 2.178 12.295 0.8370 1.017x107 3.335x107 18.6
34.0 2.314 13.064 0.8893 1.080x107 3.544x107 16.9
36.0 2.451 13.832 0.9416 1.144x107 3.752x107 15.4
38.0 2.587 14.601 0.9939 1.207x107 3.961x107 14.1
40.0 2.723 15.369 1.0462 1.271x107 4.169x107 12.8
42.0 2.859 16.138 1.0986 1.334x107 4.378x107 11.7
44.0 2.995 16.906 1.1509 1.398x107 4.586x107 10.8
46.0 3.131 17.675 1.2032 1.461x107 4.794x107 9.8
48.0 2.268 18.443 1.2555 1.525x107 5.003x107 9.0
50.0 3.404 19.212 1.3078 1.588x107 5.211x107 8.2
55.0 3.744 21.133 1.4386 1.747x107 5.732x107 6.6
60.0 4.084 23.054 1.5694 1.906x107 6.254x107 5.1
65.0 4.425 24.975 1.7001 2.065x107 6.775x107 3.9
70.0 4.765 26.896 1.8309 2.224x107 7.296x107 2.8

Performance Data for Mach 1.100

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.141 0.4861 5.776x106 1.892x107 41.6
20.0 1.361 7.934 0.5401 6.407x106 2.102x107 36.3
22.0 1.498 8.727 0.5941 7.048x106 2.312x107 32.0
24.0 1.634 9.521 0.6481 7.689x106 2.522x107 28.4
26.0 1.770 10.314 0.7021 8.389x106 2.733x107 25.4
28.0 1.906 11.108 0.7561 8.970x106 2.943x107 22.8
30.0 2.042 11.901 0.8101 9.611x106 3.153x107 20.6
32.0 2.178 12.694 0.8641 1.025x107 3.363x107 18.6
34.0 2.314 13.488 0.9182 1.089x107 3.574x107 16.9
36.0 2.451 14.281 0.9722 1.153x107 3.784x107 15.4
38.0 2.587 15.074 1.0262 1.217x107 3.994x107 14.1
40.0 2.723 15.868 1.0802 1.281x107 4.204x107 12.9
42.0 2.859 16.661 1.1342 1.345x107 4.414x107 11.7
44.0 2.995 14.455 1.1882 1.410x107 4.625x107 10.7
46.0 3.131 18.248 1.2422 1.474x107 4.835x107 9.8
48.0 2.268 19.041 1.2962 1.538x107 5.045x107 9.0
50.0 3.404 19.835 1.3502 1.602x107 5.255x107 8.2
55.0 3.744 21.818 1.4852 1.762x107 5.781x107 6.6
60.0 4.084 23.802 1.6203 1.922x107 6.306x107 5.1
65.0 4.425 25.785 1.7553 2.082x107 6.832x107 3.9
70.0 4.765 27.769 1.8903 2.242x107 7.357x107 2.8

Performance Data for Mach 1.150

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.329 0.4989 5.797x106 1.902x107 41.6
20.0 1.361 8.143 0.5544 6.441x106 2.113x107 36.3
22.0 1.498 8.958 0.6098 7.085x106 2.325x107 32.0
24.0 1.634 9.772 0.6652 7.729x106 2.536x107 28.4
26.0 1.770 10.586 0.7207 8.374x106 2.747x107 25.4
28.0 1.906 11.401 0.7761 9.018x106 2.959x107 22.8
30.0 2.042 12.215 0.8315 9.662x106 3.170x107 20.6
32.0 2.178 13.030 0.8870 1.031x107 3.381x107 18.6
34.0 2.314 13.844 0.9424 1.095x107 3.593x107 16.9
36.0 2.451 14.685 0.9978 1.159x107 3.804x107 15.4
38.0 2.587 15.473 1.0533 1.224x107 4.015x107 14.1
40.0 2.723 16.287 1.1087 1.288x107 4.227x107 12.9
42.0 2.859 17.101 1.1641 1.353x107 4.438x107 11.7
44.0 2.995 17.916 1.2196 1.417x107 4.649x107 10.7
46.0 3.131 18.730 1.2750 1.481x107 4.860x107 9.8
48.0 2.268 19.544 1.3304 1.546x107 5.072x107 9.0
50.0 3.404 20.359 1.3859 1.610x107 5.283x107 8.2
55.0 3.744 22.394 1.5245 1.771x107 5.811x107 6.6
60.0 4.084 24.430 1.6631 1.932x107 6.340x107 5.1
65.0 4.425 26.466 1.8016 2.093x107 6.868x107 3.9
70.0 4.765 28.502 1.9402 2.254x107 7.396x107 2.8

Performance Data for Mach 1.200

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.482 0.5093 5.811x106 1.907x107 41.6
20.0 1.361 8.314 0.5659 6.457x106 2.119x107 36.3
22.0 1.498 9.145 0.6225 7.103x106 2.330x107 32.0
24.0 1.634 9.976 0.6791 7.749x106 2.542x107 28.4
26.0 1.770 10.808 0.7357 8.394x106 2.754x107 25.4
28.0 1.906 11.639 0.7923 9.040x106 2.966x107 22.8
30.0 2.042 12.470 0.8489 9.686x106 3.178x107 20.6
32.0 2.178 13.302 0.9055 1.033x107 3.390x107 18.6
34.0 2.314 14.133 0.9621 1.098x107 3.601x107 16.9
36.0 2.451 14.964 1.0187 1.162x107 3.813x107 15.4
38.0 2.587 15.796 1.0753 1.227x107 4.025x107 14.1
40.0 2.723 16.627 1.1319 1.291x107 4.237x107 12.9
42.0 2.859 17.458 1.1885 1.356x107 4.449x107 11.7
44.0 2.995 18.290 1.2450 1.421x107 4.661x107 10.7
46.0 3.131 19.121 1.3016 1.485x107 4.873x107 9.8
48.0 2.268 19.952 1.3582 1.550x107 5.084x107 9.0
50.0 3.404 20.784 1.4148 1.614x107 5.296x107 8.2
55.0 3.744 22.862 1.5563 1.776x107 5.826x107 6.6
60.0 4.084 24.941 1.6978 1.937x107 6.356x107 5.1
65.0 4.425 27.019 1.8393 2.099x107 6.885x107 3.9
70.0 4.765 29.097 1.9808 2.260x107 7.415x107 2.8

Performance Data for Mach 1.250

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.601 0.5174 5.811x106 1.906x107 41.6
20.0 1.361 8.445 0.5749 6.456x106 2.118x107 36.3
22.0 1.498 9.290 0.6324 7.102x106 2.330x107 32.0
24.0 1.634 10.134 0.6899 7.748x106 2.542x107 28.4
26.0 1.770 10.979 0.7473 8.393x106 2.754x107 25.4
28.0 1.906 11.823 0.8048 9.039x106 2.966x107 22.8
30.0 2.042 12.668 0.8623 9.685x106 3.177x107 20.6
32.0 2.178 13.512 0.9198 1.033x107 3.389x107 18.7
34.0 2.314 14.357 0.9773 1.098x107 3.601x107 16.9
36.0 2.451 15.201 1.0348 1.162x107 3.813x107 15.4
38.0 2.587 16.046 1.0923 1.227x107 4.025x107 14.1
40.0 2.723 16.890 1.1498 1.291x107 4.237x107 12.8
42.0 2.859 17.737 1.2073 1.356x107 4.448x107 11.7
44.0 2.995 18.579 1.2647 1.420x107 4.660x107 10.7
46.0 3.131 19.424 1.3222 1.485x107 4.872x107 9.8
48.0 2.268 20.268 1.3797 1.550x107 5.084x107 9.0
50.0 3.404 21.113 1.4372 1.614x107 5.296x107 8.2
55.0 3.744 23.224 1.5809 1.776x107 5.825x107 6.5
60.0 4.084 25.335 1.7246 1.937x107 6.355x107 5.1
65.0 4.425 27.446 1.8646 2.098x107 6.884x107 3.9
70.0 4.765 29.558 2.0121 2.260x107 7.414x107 2.8

Performance Data for Mach 1.300

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.685 0.5232 5.796x106 1.902x107 41.6
20.0 1.361 8.539 0.5813 6.440x106 2.113x107 36.3
22.0 1.498 9.393 0.6394 7.084x106 2.324x107 32.0
24.0 1.634 10.247 0.6976 7.728x106 2.536x107 28.4
26.0 1.770 11.101 0.7557 8.372x106 2.747x107 25.4
28.0 1.906 11.955 0.8138 9.016x106 2.958x107 22.8
30.0 2.042 12.809 0.8719 9.661x106 3.169x107 20.6
32.0 2.178 13.663 0.9301 1.030x107 3.381x107 18.6
34.0 2.314 14.517 0.9882 1.095x107 3.592x107 16.9
36.0 2.451 15.371 1.0463 1.159x107 3.803x107 15.4
38.0 2.587 16.225 1.1045 1.224x107 4.015x107 14.1
40.0 2.723 17.078 1.1626 1.288x107 4.226x107 12.8
42.0 2.859 17.932 1.2207 1.352x107 4.437x107 11.7
44.0 2.995 18.786 1.2788 1.417x107 4.649x107 10.7
46.0 3.131 19.640 1.3370 1.481x107 4.860x107 9.8
48.0 2.268 20.494 1.3951 1.546x107 5.071x107 9.0
50.0 3.404 21.348 1.4532 1.510x107 5.282x107 8.2
55.0 3.744 23.483 1.5986 1.771x107 5.811x107 6.5
60.0 4.084 25.618 1.7439 1.932x107 6.339x107 5.1
65.0 4.425 27.752 1.8891 2.093x107 6.867x107 3.9
70.0 4.765 29.887 2.0345 2.254x107 7.395x107 2.8

Performance Data for Mach 1.350

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.738 0.5268 5.796x106 1.893x107 41.6
20.0 1.361 8.598 0.5853 6.410x106 2.103x107 36.3
22.0 1.498 9.458 0.6438 7.051x106 2.313x107 32.0
24.0 1.634 10.317 0.7023 7.692x106 2.524x107 28.4
26.0 1.770 11.177 0.8609 8.333x106 2.734x107 25.4
28.0 1.906 12.037 0.8194 8.974x106 2.944x107 22.8
30.0 2.042 12.897 0.8779 9.615x106 3.155x107 20.6
32.0 2.178 13.757 0.9365 1.026x107 3.365x107 18.6
34.0 2.314 14.616 0.9950 1.090x107 3.575x107 16.9
36.0 2.451 15.476 1.0535 1.154x107 3.786x107 15.4
38.0 2.587 16.336 1.1120 1.218x107 3.996x107 14.1
40.0 2.723 17.196 1.1706 1.282x107 4.206x107 12.8
42.0 2.859 18.055 1.2291 1.346x107 4.416x107 11.7
44.0 2.995 18.915 1.2876 1.410x107 4.627x107 10.7
46.0 3.131 19.775 1.3462 1.474x107 4.837x107 9.8
48.0 2.268 20.635 1.4047 1.538x107 5.047x107 9.0
50.0 3.404 21.495 1.4632 1.603x107 5.258x107 8.2
55.0 3.744 23.644 1.6095 1.763x107 5.783x107 6.5
60.0 4.084 25.793 1.7559 1.923x107 6.309x107 5.1
65.0 4.425 27.943 1.9022 2.083x107 6.835x107 3.9
70.0 4.765 30.092 2.0485 2.244x107 7.361x107 2.7

Performance Data for Mach 1.400

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.760 0.5283 5.731x106 1.880x107 41.6
20.0 1.361 8.623 0.5870 6.367x106 2.089x107 36.3
22.0 1.498 9.485 0.6457 7.004x106 2.298x107 32.0
24.0 1.634 10.347 0.7044 7.641x106 2.507x107 28.4
26.0 1.770 11.210 0.7631 8.277x106 2.716x107 25.4
28.0 1.906 12.072 0.8218 8.914x106 2.925x107 22.8
30.0 2.042 12.934 0.8805 9.551x106 3.133x107 20.6
32.0 2.178 13.796 0.9392 1.019x107 3.342x107 18.6
34.0 2.314 14.659 0.9979 1.082x107 3.551x107 16.9
36.0 2.451 15.521 1.0566 1.146x107 3.760x107 15.4
38.0 2.587 16.383 1.1153 1.210x107 3.969x107 14.1
40.0 2.723 17.246 1.1740 1.273x107 4.178x107 12.8
42.0 2.859 18.108 1.2327 1.337x107 4.387x107 11.7
44.0 2.995 18.970 1.2914 1.401x107 4.596x107 10.7
46.0 3.131 19.832 1.3501 1.464x107 4.805x107 9.8
48.0 2.268 20.695 1.4088 1.528x107 5.014x107 9.0
50.0 3.404 21.557 1.4675 1.592x107 5.222x107 8.2
55.0 3.744 23.713 1.6142 1.751x107 5.745x107 6.5
60.0 4.084 25.868 1.7609 1.910x107 6.267x107 5.1
65.0 4.425 28.024 1.9077 2.069x107 6.789x107 3.9
70.0 4.765 30.180 2.0544 2.229x107 7.311x107 2.7
Figure C - Supersonic performance Mach 1.0 - Mach 2.5.
Figure C - Supersonic performance Mach 1.0 - Mach 2.5. Long description follows.

Performance Data for Mach 1.100

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.141 0.4861 5.766x106 1.892x107 42.0
20.0 1.361 7.934 0.5401 6.407x106 2.102x107 36.6
22.0 1.498 8.727 0.5941 7.048x106 2.312x107 32.3
24.0 1.634 9.521 0.6481 7.689x106 2.522x107 28.7
26.0 1.770 10.314 0.7021 8.329x106 2.733x107 25.7
28.0 1.906 11.108 0.7561 8.970x106 2.943x107 23.1
30.0 2.042 11.901 0.8101 9.611x106 3.153x107 20.8
32.0 2.178 12.694 0.8641 1.025x107 3.363x107 18.9
34.0 2.314 13.488 0.9182 1.089x107 3.574x107 17.2
36.0 2.451 14.281 0.9722 1.153x107 3.784x107 15.6
38.0 2.587 15.074 1.0262 1.217x107 3.994x107 14.3
40.0 2.723 15.868 1.0802 1.281x107 4.204x107 13.0
42.0 2.859 16.661 1.1342 1.345x107 4.414x107 11.9
44.0 2.995 17.455 1.1882 1.410x107 4.625x107 10.9
46.0 3.131 18.248 1.2422 1.474x107 4.835x107 10.0
48.0 2.268 19.041 1.2962 1.538x107 5.045x107 9.2
50.0 3.404 19.835 1.3502 1.602x107 5.255x107 8.4
55.0 3.744 21.818 1.4852 1.762x107 5.781x107 6.7
60.0 4.084 23.802 1.6203 1.922x107 6.306x107 5.3
65.0 4.425 25.785 1.7553 2.082x107 6.832x107 4.1
70.0 4.765 27.769 1.8903 2.242x107 7.357x107 3.0

Performance Data for Mach 1.200

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.482 0.5093 5.811x106 1.907x107 43.2
20.0 1.361 8.314 0.5659 6.457x106 2.119x107 37.7
22.0 1.498 9.145 0.6225 7.103x106 2.330x107 33.3
24.0 1.634 9.976 0.6791 7.749x106 2.542x107 29.6
26.0 1.770 10.808 0.7357 8.394x106 2.754x107 26.5
28.0 1.906 11.639 0.7923 9.040x106 2.966x107 23.8
30.0 2.042 12.470 0.8489 9.686x106 3.178x107 21.5
32.0 2.178 13.302 0.9055 1.033x107 3.390x107 19.5
34.0 2.314 14.133 0.9621 1.098x107 3.601x107 17.7
36.0 2.451 14.964 1.0187 1.162x107 3.813x107 16.2
38.0 2.587 15.796 1.0753 1.227x107 4.025x107 14.8
40.0 2.723 16.627 1.1319 1.291x107 4.237x107 13.5
42.0 2.859 17.458 1.1885 1.356x107 4.449x107 12.4
44.0 2.995 18.290 1.2450 1.421x107 4.661x107 11.4
46.0 3.131 19.121 1.3016 1.485x107 4.873x107 10.4
48.0 2.268 19.952 1.3582 1.550x107 5.084x107 9.6
50.0 3.404 20.784 1.4148 1.614x107 5.296x107 8.8
55.0 3.744 22.862 1.5563 1.776x107 5.826x107 7.0
60.0 4.084 24.941 1.6978 1.937x107 6.356x107 5.6
65.0 4.425 27.019 1.8393 2.099x107 6.885x107 4.3
70.0 4.765 29.097 1.9808 2.260x107 7.415x107 3.2
75.0 5.106 31.176 2.1222 2.421x107 7.944x107 2.2

Performance Data for Mach 1.300

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.685 0.5232 5.796x106 1.902x107 45.0
20.0 1.361 8.539 0.5813 6.440x106 2.113x107 39.4
22.0 1.498 9.393 0.6394 7.084x106 2.324x107 34.8
24.0 1.634 10.247 0.6976 7.728x106 2.536x107 30.9
26.0 1.770 11.101 0.7557 8.372x106 2.747x107 27.7
28.0 1.906 11.955 0.8138 9.016x106 2.958x107 25.0
30.0 2.042 12.809 0.8719 9.661x106 3.169x107 22.6
32.0 2.178 13.663 0.9301 1.030x107 3.381x107 20.5
34.0 2.314 14.517 0.9882 1.095x107 3.592x107 18.7
36.0 2.451 15.371 1.0463 1.159x107 3.803x107 17.0
38.0 2.587 16.225 1.1045 1.224x107 4.015x107 15.6
40.0 2.723 17.078 1.1626 1.288x107 4.226x107 14.3
42.0 2.859 17.932 1.2207 1.352x107 4.437x107 13.1
44.0 2.995 18.786 1.2788 1.417x107 4.649x107 12.0
46.0 3.131 19.640 1.3370 1.481x107 4.860x107 11.1
48.0 2.268 20.494 1.3951 1.546x107 5.071x107 10.1
50.0 3.404 21.348 1.4532 1.610x107 5.282x107 9.3
55.0 3.744 23.483 1.5686 1.771x107 5.811x107 7.5
60.0 4.084 25.618 1.7439 1.932x107 6.339x107 6.0
65.0 4.425 27.752 1.8892 2.093x107 6.867x107 4.7
70.0 4.765 29.887 2.0345 2.254x107 7.395x107 3.5
75.0 5.106 32.022 2.1799 2.415x107 7.924x107 2.4

Performance Data for Mach 1.400

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.760 0.5283 5.731x106 1.880x107 47.4
20.0 1.361 8.623 0.5870 6.367x106 2.089x107 41.5
22.0 1.498 9.485 0.6457 7.004x106 2.298x107 36.7
24.0 1.634 10.347 0.7044 7.641x106 2.507x107 32.7
26.0 1.770 11.210 0.7631 8.277x106 2.716x107 29.3
28.0 1.906 12.072 0.8218 8.914x106 2.925x107 26.5
30.0 2.042 12.934 0.8805 9.551x106 3.133x107 24.0
32.0 2.178 13.796 0.9392 1.019x107 3.342x107 21.8
34.0 2.314 14.659 0.9979 1.082x107 3.551x107 19.9
36.0 2.451 15.521 1.0566 1.146x107 3.760x107 18.2
38.0 2.587 16.383 1.1153 1.210x107 3.969x107 16.7
40.0 2.723 17.246 1.1740 1.273x107 4.178x107 15.3
42.0 2.859 18.108 1.1227 1.337x107 4.387x107 14.1
44.0 2.995 18.970 1.2914 1.401x107 4.596x107 12.9
46.0 3.131 19.832 1.3501 1.464x107 4.806x107 11.9
48.0 2.268 20.695 1.4088 1.528x107 5.014x107 11.0
50.0 3.404 21.557 1.4675 1.592x107 5.222x107 10.1
55.0 3.744 23.713 1.6142 1.751x107 5.745x107 8.2
60.0 4.084 25.868 1.7609 1.910x107 6.267x107 6.6
65.0 4.425 28.024 1.9077 2.069x107 6.789x107 5.3
70.0 4.765 30.180 2.0544 2.229x107 7.311x107 4.0
75.0 5.106 32.335 2.2012 2.388x107 7.834x107 2.8

Performance Data for Mach 1.600

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
18.0 1.225 7.589 0.5166 5.483x106 1.799x107 54.6
20.0 1.361 8.432 0.5740 6.093x106 1.999x107 47.9
22.0 1.498 9.275 0.6314 6.702x106 2.199x107 42.5
24.0 1.634 10.119 0.6888 7.311x106 2.399x107 37.9
26.0 1.770 10.962 0.7462 7.921x106 2.599x107 34.1
28.0 1.906 11.805 0.8036 8.530x106 2.798x107 30.9
30.0 2.042 12.648 0.8610 9.139x106 2.998x107 28.0
32.0 2.178 13.491 0.9184 9.748x106 3.198x107 25.6
34.0 2.314 14.355 0.9758 1.036x107 3.398x107 23.4
36.0 2.451 15.178 1.0332 1.097x107 3.598x107 21.5
38.0 2.587 16.021 1.0906 1.158x107 3.798x107 19.8
40.0 2.723 16.864 1.1480 1.219x107 3.998x107 18.2
42.0 2.859 17.707 1.2054 1.279x107 4.198x107 16.8
44.0 2.995 18.551 1.2628 1.340x107 4.398x107 15.6
46.0 3.131 19.394 1.3202 1.401x107 4.598x107 14.4
48.0 2.268 20.237 1.3776 1.462x107 4.979x107 13.3
50.0 3.404 21.080 1.4350 1.523x107 4.997x107 12.4
55.0 3.744 23.188 1.5785 1.675x107 5.467x107 10.2
60.0 4.084 25.296 1.7220 1.828x107 5.997x107 8.4
65.0 4.425 27.404 1.8655 1.980x107 6.469x107 6.9
70.0 4.765 29.512 2.0090 2.132x107 6.999x107 5.5
75.0 5.106 31.620 2.1525 2.285x107 7.496x107 4.2

Performance Data for Mach 1.800

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
22.0 1.498 8.684 0.5911 6.277x106 2.059x107 50.4
24.0 1.634 9.473 0.6449 6.848x106 2.247x107 45.2
26.0 1.770 10.263 0.6986 7.418x106 2.434x107 40.8
28.0 1.906 11.052 0.7524 7.989x106 2.621x107 37.0
30.0 2.042 11.842 0.8061 8.559x106 2.808x107 33.7
32.0 2.178 12.631 0.8598 9.130x106 2.995x107 30.8
34.0 2.314 13.421 0.9136 9.701x106 3.183x107 28.3
36.0 2.451 14.210 0.9673 1.027x107 3.370x107 26.1
38.0 2.587 14.999 1.0211 1.084x107 3.557x107 24.1
40.0 2.723 15.789 1.0748 1.141x107 3.744x107 22.3
42.0 2.859 16.578 1.1285 1.198x107 3.931x107 20.7
44.0 2.995 17.368 1.1823 1.255x107 4.119x107 19.2
46.0 3.131 18.157 1.2360 1.312x107 4.306x107 17.9
48.0 2.268 18.947 1.2898 1.370x107 4.493x107 16.6
50.0 3.404 19.736 1.3435 1.427x107 4.680x107 15.5
55.0 3.744 21.710 1.4779 1.569x107 5.148x107 13.0
60.0 4.084 23.683 1.6122 1.712x107 5.616x107 11.0
65.0 4.425 25.657 1.7466 1.855x107 6.084x107 9.2
70.0 4.765 27.631 1.8809 1.997x107 6.552x107 7.6
75.0 5.106 29.604 2.0153 2.140x107 7.020x107 6.2
80.0 5.446 31.578 2.1496 2.283x107 7.489x107 4.8

Performance Data for Mach 2.000

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
24.0 1.634 8.588 0.5846 6.317x106 2.073x107 54.7
26.0 1.770 9.304 0.6334 6.844x106 2.245x107 49.4
28.0 1.906 10.020 0.6821 7.370x106 2.418x107 45.0
30.0 2.042 10.736 0.7308 7.897x106 2.591x107 41.1
32.0 2.178 11.451 0.7795 8.423x106 2.763x107 37.7
34.0 2.314 12.167 0.8282 8.950x106 2.936x107 34.8
36.0 2.451 12.883 0.8770 9.476x106 3.109x107 32.1
38.0 2.587 13.598 0.9257 1.000x107 3.282x107 29.7
40.0 2.723 14.314 0.9744 1.053x107 3.454x107 27.6
42.0 2.859 15.030 1.0231 1.106x107 3.627x107 25.7
44.0 2.995 15.746 1.0719 1.158x107 3.800x107 24.0
46.0 3.131 16.461 1.1206 1.211x107 3.972x107 22.4
48.0 2.268 17.177 1.1639 1.263x107 4.145x107 20.9
50.0 3.404 17.893 1.2180 1.316x107 4.318x107 19.6
55.0 3.744 19.682 1.3398 1.448x107 4.750x107 16.7
60.0 4.084 21.471 1.4616 1.579x107 5.182x107 14.2
65.0 4.425 23.260 1.5834 1.711x107 5.613x107 12.2
70.0 4.765 25.050 1.7052 1.843x107 6.045x107 10.4
75.0 5.106 26.839 1.8270 1.974x107 6.477x107 8.8
80.0 5.446 28.628 1.9488 2.106x107 6.909x107 7.4
85.0 5.786 30.417 2.0706 2.237x107 7.340x107 6.0
90.0 6.127 32.207 2.1924 2.369x107 7.772x107 4.6

Performance Data for Mach 2.250

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
30.0 2.042 9.194 0.6259 7.041x106 2.310x107 53.2
32.0 2.178 9.807 0.6676 7.510x106 2.464x107 49.0
34.0 2.314 10.420 0.7093 7.979x106 2.618x107 45.2
36.0 2.451 11.033 0.7510 8.449x106 2.772x107 41.9
38.0 2.587 11.646 0.7928 8.918x106 2.926x107 39.0
40.0 2.723 12.259 0.8345 9.388x106 3.080x107 36.3
42.0 2.859 12.872 0.8762 9.857x106 3.234x107 33.9
44.0 2.995 13.485 0.9179 1.033x107 3.388x107 31.7
46.0 3.131 14.098 0.9597 1.080x107 3.542x107 29.7
48.0 2.268 14.711 1.0014 1.127x107 3.696x107 27.9
50.0 3.404 15.323 1.0431 1.173x107 3.850x107 26.2
55.0 3.744 16.856 1.1474 1.291x107 4.235x107 22.6
60.0 4.084 18.388 1.2517 1.408x107 4.620x107 19.6
65.0 4.425 19.921 1.3561 1.525x107 5.005x107 17.0
70.0 4.765 21.453 1.4604 1.643x107 5.390x107 14.8
75.0 5.106 22.985 1.5647 1.760x107 5.775x107 12.9
80.0 5.446 24.518 1.6690 1.878x107 6.160x107 11.2
85.0 5.786 26.050 1.7733 1.995x107 6.545x107 9.6
90.0 6.127 27.582 1.8776 2.112x107 6.930x107 8.3
95.0 6.467 29.115 1.9819 2.230x107 7.315x107 7.0
100.0 6.807 30.647 2.0862 2.347x107 7.700x107 5.7
105.0 7.148 32.179 2.1906 2.464x107 8.085x107 4.4

Performance Data for Mach 2.500

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
36.0 2.451 9.218 0.6275 7.463x106 2.449x107 54.9
38.0 2.587 9.730 0.6624 7.878x106 2.585x107 51.1
40.0 2.723 10.242 0.6972 8.292x106 2.721x107 47.7
42.0 2.859 10.754 0.7321 8.707x106 2.857x107 44.7
44.0 2.995 11.267 0.7670 9.122x106 2.993x107 41.9
46.0 3.131 11.779 0.8018 9.536x106 3.129x107 39.4
48.0 2.268 12.291 0.8367 9.951x106 3.265x107 37.0
50.0 3.404 12.803 0.8715 1.037x107 3.401x107 34.9
55.0 3.744 14.083 0.9587 1.140x107 3.741x107 30.3
60.0 4.084 15.363 1.0458 1.244x107 4.081x107 26.5
65.0 4.425 16.644 1.1330 1.348x107 4.421x107 23.2
70.0 4.765 17.924 1.2202 1.451x107 4.761x107 20.4
75.0 5.106 19.204 1.3073 1.555x107 5.101x107 18.0
80.0 5.446 20.485 1.3945 1.658x107 5.441x107 15.9
85.0 5.786 21.765 1.4816 1.761x107 5.781x107 14.0
90.0 6.127 23.045 1.5688 1.866x107 6.121x107 12.4
95.0 6.467 24.326 1.6559 1.969x107 6.461x107 10.9
100.0 6.807 25.606 1.7431 2.073x107 6.802x107 9.5
105.0 7.148 26.886 1.8302 2.177x107 7.142x107 8.2
110.0 7.488 28.166 1.9174 2.280x107 7.482x107 7.0
115.0 7.828 29.447 2.0045 2.384x107 7.822x107 5.9
120.0 8.169 30.727 2.0917 2.488x107 8.162x107 4.8
125.0 8.509 32.007 2.1788 2.591x107 8.502x107 3.6
Figure D - Supersonic performance Mach 2.0 - Mach 5.0.
Figure D - Supersonic performance Mach 2.0 - Mach 5.0. Long description follows.

Performance Data for Mach 2.750

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
46.0 3.131 9.686 0.6594 8.386x106 2.751x107 51.8
48.0 2.268 10.107 0.6880 8.750x106 2.871x107 48.8
50.0 3.404 10.528 0.7167 9.115x106 2.990x107 46.1
55.0 3.744 11.581 0.7884 1.003x107 3.290x107 40.2
60.0 4.084 12.634 0.8600 1.094x107 3.589x107 35.3
65.0 4.425 13.687 0.9317 1.185x107 3.888x107 31.2
70.0 4.765 14.740 1.0034 1.276x107 4.187x107 27.7
75.0 5.106 15.793 1.0751 1.367x107 4.486x107 24.6
80.0 5.446 16.845 1.1467 1.458x107 4.785x107 21.9
85.0 5.786 17.898 1.2184 1.550x107 5.084x107 19.6
90.0 6.127 18.951 1.2901 1.641x107 5.383x107 17.5
95.0 6.467 20.004 1.3617 1.732x107 5.682x107 15.6
100.0 6.807 21.057 1.4334 1.823x107 5.981x107 13.9
105.0 7.148 22.110 1.5051 1.914x107 6.280x107 12.4
110.0 7.488 23.162 1.5767 2.005x107 6.579x107 11.0
115.0 7.828 24.215 1.6484 2.096x107 6.878x107 9.7
120.0 8.169 25.268 1.7201 2.188x107 7.177x107 8.8
125.0 8.509 26.321 1.7918 2.279x107 7.476x107 7.4
130.0 8.850 27.374 1.8634 2.370x107 7.775x107 6.4
135.0 9.190 28.427 1.9351 2.461x107 8.074x107 5.4
140.0 9.530 29.479 2.0068 2.552x107 8.373x107 4.4
145.0 9.871 30.532 2.0784 2.643x107 8.672x107 3.4
150.0 10.211 31.585 2.1501 2.735x107 8.971x107 2.4

Performance Data for Mach 3.000

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
60.0 4.084 10.291 0.7005 9.606x106 3.152x107 46.6
65.0 4.425 11.148 0.7589 1.041x107 3.414x107 41.4
70.0 4.765 12.006 0.8173 1.121x107 3.677x107 36.8
75.0 5.106 12.863 0.8756 1.201x107 3.940x107 33.0
80.0 5.446 13.721 0.8340 1.281x107 4.202x107 29.5
85.0 5.786 14.578 0.9924 1.361x107 4.465x107 26.6
90.0 6.127 15.436 1.0508 1.441x107 4.727x107 23.9
95.0 6.467 16.293 1.1091 1.521x107 4.990x107 21.6
100.0 6.807 17.151 1.1675 1.601x107 5.253x107 19.4
105.0 7.148 18.008 1.2259 1.681x107 5.515x107 17.5
110.0 7.488 18.866 1.2843 1.761x107 5.778x107 15.7
115.0 7.828 19.724 1.3427 1.841x107 6.041x107 14.2
120.0 8.169 20.581 1.4010 1.921x107 6.303x107 12.7
125.0 8.509 21.439 1.4594 2.001x107 6.566x107 11.4
130.0 8.850 22.296 1.5178 2.081x107 6.829x107 10.1
135.0 9.190 23.154 1.5762 2.161x107 7.091x107 9.0
140.0 9.530 24.011 1.6345 2.241x107 7.354x107 7.9
145.0 9.871 24.869 1.6929 2.322x107 7.616x107 6.9
150.0 10.211 25.726 1.7513 2.402x107 7.879x107 6.0
155.0 10.551 26.584 1.8097 2.482x107 8.142x107 5.0
160.0 10.892 27.442 1.8680 2.562x107 8.404x107 4.1
165.0 11.232 28.299 1.8264 2.642x107 8.667x107 3.3
170.0 11.572 29.157 1.9848 2.722x107 8.930x107 2.6

Performance Data for Mach 3.250

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
75.0 5.106 10.424 0.7096 1.056x107 3.463x107 43.5
80.0 5.446 11.119 0.7569 1.126x107 3.694x107 39.2
85.0 5.786 11.814 0.8042 1.196x107 3.925x107 35.4
90.0 6.127 12.509 0.8515 1.267x107 4.156x107 32.0
95.0 6.467 13.204 0.8988 1.337x107 4.387x107 29.0
100.0 6.807 13.899 0.8462 1.407x107 4.617x107 26.4
105.0 7.148 14.594 0.9935 1.478x107 4.848x107 23.9
110.0 7.488 15.289 1.0408 1.548x107 5.079x107 21.7
115.0 7.828 15.984 1.0881 1.619x107 5.310x107 19.7
120.0 8.169 16.679 1.1354 1.689x107 5.751x107 17.9
125.0 8.509 17.374 1.1827 1.759x107 5.772x107 16.2
130.0 8.850 18.069 1.2300 1.830x107 6.003x107 14.6
135.0 9.190 18.764 1.2773 1.900x107 6.234x107 13.2
140.0 9.530 19.459 1.3246 1.970x107 6.466x107 11.9
145.0 9.871 20.153 1.3719 2.041x107 6.695x107 10.7
150.0 10.211 20.848 1.4192 2.111x107 6.926x107 9.5
155.0 10.551 21.543 1.4665 2.181x107 7.157x107 8.4
160.0 10.892 22.238 1.5138 2.252x107 7.388x107 7.4
165.0 11.232 22.933 1.5611 2.322x107 7.619x107 6.5
170.0 11.572 23.628 1.6085 2.393x107 7.850x107 5.6
175.0 11.913 24.323 1.6558 2.463x107 8.081x107 4.8
180.0 12.253 25.018 1.7031 2.533x107 8.311x107 4.0
185.0 12.594 25.713 1.7504 2.604x107 8.542x107 3.3
190.0 12.934 26.408 1.7977 2.674x107 8.773x107 2.6

Performance Data for Mach 3.500

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
80.0 5.446 8.994 0.6123 9.921x106 3.255x107 51.1
85.0 5.786 9.556 0.6505 1.054x107 3.458x107 46.2
90.0 6.127 10.118 0.6888 1.116x107 3.662x107 42.0
95.0 6.467 10.680 0.7271 1.178x107 3.865x107 38.1
100.0 6.807 11.243 0.7653 1.240x107 4.069x107 34.6
105.0 7.148 11.805 0.8036 1.302x107 4.272x107 31.6
110.0 7.488 12.367 0.8419 1.364x107 4.476x107 28.8
115.0 7.828 12.929 0.8801 1.426x107 4.679x107 26.2
120.0 8.169 136491 0.8184 1.488x107 4.882x107 23.8
125.0 8.509 14.053 0.8567 1.550x107 5.086x107 21.7
130.0 8.850 14.615 0.9949 1.612x107 5.289x107 19.8
135.0 9.190 15.178 1.0332 1.674x107 5.493x107 18.0
140.0 9.530 15.740 1.0715 1.736x107 5.696x107 16.3
145.0 9.871 16.302 1.1097 1.798x107 5.900x107 14.7
150.0 10.211 16.864 1.1480 1.860x107 6.103x107 13.2
155.0 10.551 17.426 1.1863 1.922x107 6.306x107 11.9
160.0 10.892 17.988 1.2245 1.984x107 6.510x107 10.5
165.0 11.232 18.550 1.2628 2.046x107 6.713x107 9.4
170.0 11.572 19.112 1.3011 2.108x107 6.917x107 8.2
175.0 11.913 19.675 1.3393 2.170x107 7.120x107 7.2
180.0 12.253 20.237 1.3776 2.232x107 7.324x107 6.2
185.0 12.594 20.799 1.4158 2.294x107 7.527x107 5.3
190.0 12.934 21.361 1.4541 2.356x107 7.731x107 4.4
195.0 13.615 21.923 1.4924 2.418x107 7.934x107 3.5
200.0 13.615 22.485 1.5306 2.480x107 8.137x107 2.7

Performance Data for Mach 3.750

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
120.0 8.169 10.917 0.7432 1.316x107 4.316x107 31.1
125.0 8.509 11.372 0.7741 1.370x107 4.496x107 28.4
130.0 8.850 11.827 0.8051 1.425x107 4.676x107 25.9
135.0 9.190 12.282 0.8361 1.480x107 4.856x107 23.6
140.0 9.530 12.737 0.8670 1.535x107 5.036x107 21.5
145.0 9.871 13.191 0.8980 1.590x107 5.216x107 19.5
150.0 10.211 13.646 0.9290 1.645x107 5.395x107 17.7
155.0 10.551 14.101 0.9599 1.699x107 5.575x107 15.9
160.0 10.892 14.556 0.9909 1.754x107 5.755x107 14.3
165.0 11.232 15.011 1.0219 1.809x107 5.935x107 12.8
170.0 11.572 15.466 1.0528 1.864x107 6.115x107 11.4
175.0 11.913 15.921 1.0838 1.919x107 6.295x107 10.1
180.0 12.253 16.376 1.1147 1.973x107 6.475x107 8.8
185.0 12.594 16.831 1.1457 2.028x107 6.654x107 7.6
190.0 12.934 17.285 1.1767 2.083x107 6.834x107 6.5
195.0 13.615 17.740 1.2076 2.138x107 7.014x107 5.5
200.0 13.615 18.195 1.2386 2.193x107 7.194x107 4.5
205.0 13.955 19.650 1.2696 2.248x107 7.374x107 3.5
210.0 14.295 19.105 1.3005 2.302x107 7.554x107 2.6

Performance Data for Mach 4.000

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
155.0 10.551 11.433 0.7783 1.508x107 4.948x107 21.2
160.0 10.892 11.802 0.8034 1.557x107 5.107x107 19.2
165.0 11.232 12.171 0.8285 1.605x107 5.267x107 17.2
170.0 11.572 12.540 0.8536 1.654x107 5.427x107 15.4
175.0 11.913 12.909 0.8787 1.703x107 5.586x107 13.7
180.0 12.253 13.278 0.9038 1.751x107 5.746x107 12.2
185.0 12.594 13.646 0.9290 1.800x107 5.906x107 10.7
190.0 12.934 14.015 0.9541 1.849x107 6.065x107 9.2
195.0 13.615 14.384 0.9792 1.897x107 6.225x107 7.9
200.0 13.615 14.753 1.0043 1.946x107 6.384x107 6.6
205.0 13.955 15.122 1.0294 1.995x107 6.544x107 5.4
210.0 14.295 15.490 1.0545 2.043x107 6.704x107 4.3
215.0 14.636 15.859 1.0796 2.092x107 6.863x107 3.2
220.0 14.976 16.228 1.1047 2.141x107 7.023x107 2.2

Performance Data for Mach 4.250

Total Pressure Dynamic Pressure Unit Reynolds Number Useful Run Time
psia ATMOS psia ATMOS per foot per meter Secs
170.0 11.572 10.199 0.6943 1.474x107 4.836x107 20.4
175.0 11.913 10.499 0.7147 1.517x107 4.978x107 18.3
180.0 12.253 10.799 0.7351 1.561x107 5.120x107 16.3
185.0 12.594 11.099 0.7555 1.604x107 5.263x107 14.4
190.0 12.934 11.399 0.7759 1.647x107 5.405x107 12.6
195.0 13.615 11.699 0.7964 1.691x107 5.547x107 10.9
200.0 13.615 11.999 0.8168 1.734x107 5.689x107 9.3
205.0 13.955 12.298 0.8372 1.777x107 5.831x107 7.8
210.0 14.295 12.598 0.8576 1.821x107 5.974x107 6.3
215.0 14.636 12.898 0.8780 1.864x107 6.116x107 5.0
220.0 14.976 13.198 0.8985 1.907x107 6.258x107 3.6
225.0 15.317 13.498 0.9189 1.951x107 6.400x107 2.4

Test support

  • Wind tunnel test project planning and coordination
  • Wind tunnel test optimization
  • Model design and manufacture
  • Advanced wind tunnel test technique development
  • Data analysis
  • Computational fluid dynamics (CFD)

Citations for technical papers

  • [1] A. Toledano, J. Weiss, F. Morency, C. Broughton and A. Benmeddour, "Study of the subsonic wall interference in stall of the NASA CRM at the NRC 1.5 m Trisonic Wind Tunnel," in 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, USA, 2017.
  • [2] A. Toledano, J. Weiss, F. Morency, C. Broughton and A. Benmeddour, "Towards the use of CFD to improve and validate the wall correction methodology at the NRC 1.5 m trisonic wind tunnel," in 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Washington, USA, 2016.
  • [3] Y. Mebarki, "Pressure-sensitive paint measurements on a moving store in the NRC 1.5 m blowdown wind tunnel," in 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Washington, USA, 2016.
  • [4] Y. Mebarki, B. Lascombes, L. Ferracina and J. Underwood, "Development of Pressure-Sensitive Paints for Flexible Parachutes," in 23rd AIAA Aerodynamic Decelerator Systems Technology Conference, Daytona Beach, FL, USA, 2015.
  • [5] J. Kuzub, Y. Mebarki and A. Whitehead, "Improved pressure sensitive paint measurement using natural feature tracking and piecewise linear resection," in 8th Canadian Conference on Computer and Robot Vision, CRV 2011, St. Johns, Canada, 2011.
  • [6] M. Grenier and F. Tang, "Wind Tunnel Investigation of the Effects of FLIR Pod and AIM-7 to Adjacent Stores on the CF-18 Aircraft using PSP," in 26th Congress of International Council of the Aeronautical Sciences, Anchorage, USA, 2008.
  • [7] M. Van Der Steen, D. Orchard and F. Tang, "The Application of Semi-Empirical Store Release Simulation for the Optimization of Grid Survey Wind Tunnel Testing," in International Council of the Aeronautical Sciences (ICAS) 2008 Congress, Anchorage, Alaska, USA, 2008.
  • [8] S. McIlwain and N. Tang, "Aerodynamic Effects of Different FLIR Pods Carried by the CF-18 Aircraft," in 26th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii, USA, 2008.
  • [9] D. Orchard, B. Lee and F. Tang, "Influence of Captive Stores on the Unsteady Pressure Distribution within a Rectangular Cavity," in 25th Congress of the International Council of the Aerospace Sciences, Hamburg, Germany, 2006.
  • [10] Y. Mebarki, M. Grenier, F. Ellis, J. Bureau, D. Orchard and F. Tang, "Study of the Flow around an External Fuel Tank Mounted under a CF-18 Wing using Combined PSP and Schlieren Techniques," in 23rd AIAA Applied Aerodynamics Conference, Toronto, Canada, 2005.
  • [11] Y. Mebarki, M. Grenier, F. Ellis, J. Bureau, D. Orchard, F. Tang and J. Thain, "Combination of Pressure Sensitive Paint and Schlieren Techniques in the 1.5m Trisonic Blowdown Wind Tunnel," in 101st Meeting of the Supersonic Tunnel Association, Ronkonkoma, USA, 2004.
  • [12] L. Ohman, V. Nguyen, F. Ellis, J. Thain, N. Tang, C. Broughton, Y. Mebarki, J. Fincer and J. Bureau, "The IAR 1.5m Trisonic Blowdown Wind Tunnel: A Review of its History and Development," Canadian Aerospace Journal, 28 October 2003.
  • [13] D. Orchard, M. Ahmadi and F. Tang, "Store Separation Simulations and its Application to CTS System Design," in RAeS Aerospace Aerodynamics Research Conference 2003, London, UK, 2003.
  • [14] A. Benmeddour, F. Fortin and F. Tang, "PSP Validation of the CFD Predicted CF-18/MK-83 BSU-85 Mutual Interference," in CASI 9TH Aerodynamics Symposium, Montreal, Canada, 2003.
  • [15] D. Orchard and M. Ahmadi, "Enhancement of Store Separation Wind Tunnel Testing Using Virtual Reality Visualization," in International Test and Evaluation Association: Aircraft-Stores Compatibility Symposium XIII, Destin, USA, 2003.
  • [16] A. Rebaine, M. Khalid, C. Broughton and F. Ellis, "Numerical and Experimental Investigation of the Flowfield in a Blowdown Wind Tunnel Contraction and Nozzle," in CFD 2002, Windsor, Canada, 2002.
  • [17] A. Rebaine, M. Khalid, C. Broughton and F. Ellis, "Numerical and Experimental Investigation of the Flowfield in a Blow Down Wind Tunnel," in ICAS 2002: 23rd International Congress of Aeronautical Sciences, Toronto, Canada, 2002.
  • [18] A. Benmeddour, F. Fortin and F. Tang, "CFD Study of the Sting Support Interference Effects on Store Separation Characteristics," in CEAS Aerospace Aerodynamics Research Conference, Cambridge, UK, 2002.
  • [19] Y. Mebarki and Y. Le Sant, "Pressure Sensitive Paint Evaluation on a Supercritical Wing at Cruise Speed," Journal of Visualization, vol. 4, no. 4, pp. 313-322, 2001.
  • [20] Y. Mebarki, V. Nguyen and J. Thain, "Pressure Sensitive Paint Application on a CAST10-2/DOA2 Supercritical Airfoil at Transonic Speed," in CASI 8th Aerodynamics Symposium, Toronto, Canada, 2001.
  • [21] A. Rebaine, M. Khalid, C. Broughton and F. Ellis, "Numerical Flow Simulation of a Blow Down Wind Tunnel Control Valve Wide Angle Diffuser with Comparison to Scaled Experimental Model," in CASI 48th Annual Conference: 8th Aerodynamics Symposium, Toronto, Canada, 2001.
  • [22] L. Jiang, F. Tang and L. Ohman, "Transonic flow-field around the CF-18 wing at angle of attack 4.5 degrees," in CASI 46th Conference, 1999.
  • [23] A. Benmeddour, L. Ohman, F. Fortin and D. Jones, "Comparison of Experimental Flow Field Data with CFD Predictions for the CF-18 Aircraft with the 330 EFT Mounted," in Proceedings of the Supersonic Tunnel Association International 90th Meeting, Ottawa, Canada, 1998.

Fees

We offer fee-for-service testing in all of our wind tunnel testing facilities at competitive rates that include the support of technical experts, research officers and engineers. Depending on the nature of a client's request, we also offer research and business opportunities that can translate into collaborative agreements or consortia work. Contact us to discuss your options and develop a customized plan to fit your technology needs.

Targeted industries

Aerospace, automotive and surface transportation, construction, energy.

Contact us

Dean Flanagan, Client Relationship Leader
Telephone: 613-990-8319
Email: Dean.Flanagan@nrc-cnrc.gc.ca

Related information

Aerospace Research Centre

Gallery

Date modified: