Pressure fluctuations underlying attached and separated supersonic turbulent boundary layers and shock waves-Reference-Cited by-同舟云学术

Pressure fluctuations underlying attached and separated supersonic turbulent boundary layers and shock waves

Published:1973-08-16 Issue: Volume: Page:
ISSN:
Container-title:Aeroacoustics Conference
language:
Short-container-title:

Author:

COE C.¹,CHYU W.¹,DODS, JR. J.¹

Affiliation:

1. NASA, Ames Research Center,Moffett Field, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1973-996

Reference16 articles.

1. Aeroacoustic Environments on Prospective Space Shuttle Vehicles," TM X-2570, July 1972, NASA. 2peaker,W. F. and Ailman, C. M. "Spectra and

2. Space-time Correlations of the Fluctuating Pressures at a Wall Beneath a Supersonic Turbulent Boundary Layer Perturbed by Steps and Shock Waves," Douglas Rept. SM-49806, Nov. 1965. 3owson,M. V. "Prediction of the Inflight Fluc

3. G (f)um/d6 = expi-8.094 - 1.239- 0.295x2 P 4hyu,W. J. and Hanly, R. D. "Power- and Cross

4. Spectra and Space-Time Correlations of Surface - 0.090x3 - 0.014x4 - 0.001x5) (7) Fluctuating Pressures at Mach Numbers Between

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