Over-expansion effects on Mach 3.0 supersonic jet acoustics

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

Volumn , Issue , 2008, Pages

  Nonomura, Taku ^a,c   Fujii, Kozo ^b,c  

^a UNIVERSITY OF TOKYO   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c Department of Aeronautics and Astronautics ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVES; AEROACOUSTICS; AVIATION; EXPANSION; LARGE EDDY SIMULATION; REYNOLDS NUMBER; ROCKETS; SUPERSONIC AERODYNAMICS;

COMPACT SCHEMES; COMPUTATIONAL COSTS; COMPUTATIONAL RESULTS; EXPANSION EFFECT; HIGH MACH NUMBER; LOW MACH NUMBERS; MACH WAVE EMISSION; MONOTONICALLY INTEGRATED LARGE-EDDY SIMULATIONS;

MACH NUMBER;

EID: 78249231722     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-2836     Document Type: Conference Paper

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