Validation of Computational Fluid Dynamics for supersonic Shock containing jets

14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)

Volumn , Issue , 2008, Pages

  Miller, Steven A E ^a,b   Veltin, Jérémy ^a,b   Morris, Philip J ^a,b   McLaughlin, Dennis K ^a,b  

^a PENNSYLVANIA STATE UNIVERSITY   (United States)

^b 233 Hammond Building ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXISYMMETRIC; AXISYMMETRIC NOZZLES; CONTOUR PLOT; DESIGN PARAMETERS; MODEL DEVELOPMENT; PITOT PRESSURE; QUALITATIVE ASSESSMENTS; REYNOLDS-AVERAGED NAVIER-STOKES; SHOCK ASSOCIATED NOISE; SHOCK NOISE; STATIC PRESSURE; STEADY STATE; SUPERSONIC JETS; TWO-EQUATION TURBULENCE MODELS;

COMPUTATIONAL FLUID DYNAMICS; EQUATIONS OF STATE; FLUID DYNAMICS; GAS DYNAMICS; MACH NUMBER; NAVIER STOKES EQUATIONS; SUPERSONIC AERODYNAMICS; TURBULENCE MODELS;

AEROACOUSTICS;

EID: 78249280775     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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