Advances in understanding supersonic jet screech
Author:
Affiliation:
1. NASA, Lewis Research Center, Brook Park, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-279
Reference249 articles.
1. A Note on the Coupling Between Flow Instabilities and Incident Sound
2. Ahuja, K.K.,Lepicovsky, J., Tarn, C.K.W., Morris,P.J. & Burrin, R.H. 1982 Tone excited jet - theory and experiments. NASA CR 3538.
3. Ahuja, K.K. 1984 Basic experimental study of the coupling between flow instabilities and incident sound. NASA CR 3789.
4. Ahuja, K.K.& Lepicovsky, J. 1986 Some unresolved questions on hot-jet mixing control through artificial excitation.,AIAA Paper 86-1956.
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