Acoustic Wave Generation in a Compressible Wake-Reference-Cited by-同舟云学术

Acoustic Wave Generation in a Compressible Wake

Published:2006 Issue:4 Volume:49 Page:1086-1091
ISSN:1340-8054
Container-title:JSME International Journal Series B
language:en
Short-container-title:JSME international journal. Ser. B, Fluids and thermal engineering

Author:

MAEKAWA Hiroshi¹,TAKIGUCHI Takashi¹,WATANABE Daisuke¹

Affiliation:

1. Graduate School of Engineering, Hiroshima University

Publisher

Japan Society of Mechanical Engineers

Subject

Fluid Flow and Transfer Processes,Physical and Theoretical Chemistry,Mechanical Engineering

Link

http://www.jstage.jst.go.jp/article/jsmeb/49/4/49_4_1086/_pdf

Reference15 articles.

1. (1) Lele, S.K. and Moin, P., Direct Simulation of a Mach 1.92 Jet and Its Sound Field, 4th AIAA/CEAS Aeroacoustic Conference, No.98-2291 (1998), pp.1-12.

2. Sound generation in a mixing layer

3. Direct computation of the sound generated by vortex pairing in an axisymmetric jet

4. (4) Sandham, N.D. and Reynolds, W.C., A Numerical Investigation of the Compressible Mixing Layer, Mechanical Engineering Department, Stanford Univ., Stanford, CA, Rept. TF-45, (1989).

5. The effect of Mach number on the stability of a plane supersonic wake

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