Numerical simulations of shock-vortex interactions in supersonic jet screech

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Manning, Ted A ^a   Lele, Sanjiva K ^a,b  

^a 496 Lomita Mall   (United States)

^b STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; ACOUSTIC WAVES; AIRCRAFT ACCIDENTS; AIRCRAFT MANUFACTURE; AIRFRAMES; NUMERICAL MODELS; SHOCK WAVES; SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT; VORTEX FLOW;

ACOUSTIC PRESSURE AMPLITUDE; AIRCRAFT STRUCTURE; DISCONTINUITY CAPTURING; ESSENTIALLY NON-OSCILLATORY; ISENTROPIC COMPRESSION; NON REFLECTING BOUNDARY CONDITION; SHOCK-VORTEX INTERACTION; VORTICITY THICKNESS;

SHEAR FLOW;

EID: 85088748572     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-282     Document Type: Conference Paper

References (19)

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