Computational Analysis of the Effect of Porosity on Shock Cell Strength at Cruise
Author:
Affiliation:
1. Eagle Aeronautics, Inc.
2. Analytical Services and Materials, Inc.
3. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2468
Reference15 articles.
1. 2Long,D.F.“EffectofNozzleGeometryonTurbofanShockCellNoiseatCruise,”AIAAPaper2005-0998,May2005.
2. 3Harper-Bourne,M.andFisher,M.J.“TheNoisefromShockWavesinSupersonicJets,”AGARD-CP-131,1974.
3. 4Pao, S. P. and Seiner, J. M. “A Theoretical and Experimental Investigation of Shock-Associated Noise in Supersonic Jets,” AIAA Paper 1981-1973,Oct.1981.
4. Multiscale turbulence effects in underexpanded supersonic jets
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