Underexpanded screeching jets from circular, rectangular and elliptic nozzles
Author:
Affiliation:
1. Modern Technologies Corp., Middleburg Heights, OH
2. NYMA, Inc., Brook Park, OH
3. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1623
Reference9 articles.
1. In-flight shock cell noise
2. 2Cain, A. B., Bower, W. W., Walker, S. H. & Lockwood, M. K. 1995 Modeling supersonic jet screech Part 1: vortical instability wave modeling. AIAA paper 95-0506.
3. 3Panda, J. June 1995a Measurement of shock oscillation in underexpanded supersonic jets. AIAA paper 95-2145.
4. On the Noise Emanating from a Two-Dimensional Jet Above the Critical Pressure
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