Prediction method for broadband shock-associated noise from supersonic rectangular jets

Journal of Aircraft

Volumn 33, Issue 2, 1996, Pages 298-303

  Tam, Christopher K W ^a,c,d   Reddy, N N ^b,d  

^a FLORIDA STATE UNIVERSITY   (United States)

^b LOCKHEED MARTIN   (United States)

^c Lockheed Martin Corporation   (United States)

^d AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ASPECT RATIO; CALCULATIONS; FLIGHT DYNAMICS; FLOW OF FLUIDS; MATHEMATICAL MODELS; NOZZLES; SUPERSONIC AIRCRAFT; TURBULENCE;

BROADBAND SHOCK ASSOCIATED NOISE; MACH NUMBER; PREDICTION METHOD; SHOCK CELL SYSTEMS; SUPERSONIC JETS;

JET AIRCRAFT;

EID: 0030109219     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46937     Document Type: Article

References (16)

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