Shear Layer Corrections for Non-Axisymmetric Wind Tunnel and Applications
Author:
Affiliation:
1. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2260
Reference43 articles.
1. Von Glahn, U., Groesbeck, D., and Goodykoontz, J. "Velocity Decay and Acoustic Characteristics of VariousNozzle Geometries in ForwardFlight,"AIAApaper73-629,1973.
2. Cocking, B. J., and Bryce, W. D. "Subsonic Jet Noise in Flight Based on Some Recent Wind Tunnel Results,"AIAApaper75-462,1974.
3. Bushell,K.W. "Measurement and PredictionofJet Noise in Flight,"AIAA Paper75-461,1975.
4. Packman, A. B., Ng, K. W., and Paterson, R. W. "Effect of Simulated Forward Flight on Subsonic Jet ExhaustNoise", AIAApaper75-869,1975.
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