Research relevant to problem of intense noise generated by modern jet propelled aircraft; various arrangements of both subsonic and supersonic jets used; typical shadowgraphs; when shock and jet impinged against each other head on, intense, intermittent, and h-f acoustic radiation manifested itself on flow field behind shock front; explanations of phenomenon.
Experiments on interaction between traveling shock wave and turbulent jet
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 24 , n 11
1957
7 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Comparison of data from two shock wave-turbulent boundary layer interaction experiments
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