A numerical study of nozzle boundary layer thickness on axisymmetric supersonic jet screech tones

Collection of Technical Papers - 12th AIAA/CEAS Aeroacoustics Conference

Volumn 6, Issue , 2006, Pages 3580-3591

  Gao, J H ^a,b   Li, X D ^a,b,c  

^a BEIHANG UNIVERSITY   (China)

^b BUAA   (China)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC VARIABLES CONTROL; DISPERSION (WAVES); JETS; NOZZLES; SUPERSONIC AERODYNAMICS;

CURVILINEAR COORDINATE SYSTEMS; NOZZLE BOUNDARY LAYERS; RUNGE-KUTTA SCHEME; SUPERSONIC JETS;

BOUNDARY LAYERS;

EID: 33845618548     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-2675     Document Type: Conference Paper

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