Numerical prediction of chevron nozzle noise reduction using WIND-MGBK methodology

Collection of Technical Papers - 10th AIAA/CEAS Aeroacoustics Conference

Volumn 3, Issue , 2004, Pages 2036-2054

  Engblom, W A ^a,b   Khavaran, A ^a,c   Bridges, J ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

^b AEROSPACE CORPORATION   (United States)

^c QSS ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EFFECTIVE PERCEIVED NOISE LEVEL (EPNL); JET ENGINE NOISE; REYNOLDS AVERAGED NAVIER STOKES (RANS); SMALL HOT JET ACOUSTIC RIG (SHJAR);

COMPUTER HARDWARE; JET ENGINES; JETS; KINETIC ENERGY; NAVIER STOKES EQUATIONS; NOZZLES; REYNOLDS NUMBER; ROBUSTNESS (CONTROL SYSTEMS); TURBULENCE; TURBULENT FLOW;

NOISE ABATEMENT;

EID: 19944393568     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

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