The direct computation of mach wave radiation in an axisymmetric supersonic jet

2nd AIAA/CEAS Aeroacoustics Conference

Volumn , Issue , 1996, Pages

  Mitchell, Brian E ^a,b   Lele, Sanjiva K ^c   Moin, Parviz ^a  

^a Stanford University   (United States)

^b GE GLOBAL RESEARCH   (United States)

^c 496 Lomita Mall   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; COMPUTATION THEORY; COMPUTATIONAL METHODS; FIGHTER AIRCRAFT; FORECASTING; SHEAR FLOW; SUPERSONIC AERODYNAMICS;

AXISYMMETRIC JET; COMPRESSIBLE NAVIER-STOKES EQUATIONS; COMPUTATIONAL DOMAINS; DIRECT COMPUTATIONS; FAR-FIELD SOUND; LINEAR INSTABILITY WAVES; LINEAR STABILITY THEORY; MACH WAVE RADIATION;

NAVIER STOKES EQUATIONS;

EID: 84977107099     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1729     Document Type: Conference Paper

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