Nonlinear effects on sound in nearly sonic duct flows
Author:
Affiliation:
1. Advanced Analytical Research, Inc., New York, N.Y.
2. George Washington University, Joint Institute for Advancement of Flight Sciences, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-1296
Reference7 articles.
1. the Singular Behavior of Linear ACOUStic Theory i n Near-Sonic Duct Flows", Journal of Sound and Vibration, 51(4), Ap r i l 22,1977, pp.517-531. 3. Van Dyke,M., Perturbation Methodsi n
2. I = -(l-Nj 2in V [F(-v,l;)-F(-z;)l, 1 -2N 3 -2N 1 0 2 1-X
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Shock development in sound transmitted through a nearly choked flow;7th Aeroacoustics Conference;1981-08-17
2. Acoustic shocks in nearly choked duct flows;6th Aeroacoustics Conference;1980-06-04
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