Computational analysis of a chevron nozzle uniquely tailored for propulsion airframe aeroacoustics

Collection of Technical Papers - 12th AIAA/CEAS Aeroacoustics Conference

Volumn 1, Issue , 2006, Pages 495-517

  Massey, Steven J ^a,e,f   Elmiligui, Alaa A ^b,e,f   Hunter, Craig A ^c,g   Thomas, Russell H ^c,f,h   Pao, S Paul ^c,f,g   Mengle, Vinod G ^d,f,i  

^a Eagle Aeronautics Inc   (United States)

^b ANALYTICAL SERVICES AND MATERIALS INC   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

^d BOEING COMPANY   (United States)

^e AIAA ^*

^f AIAA   (United States)

^g Building 45   (United States)

^h Aeroacoustics Branch   (United States)

ⁱ Acoustics and Fluid Mechanics

Author keywords

[No Author keywords available]

Indexed keywords

AZIMUTHALLY VARYING CHEVRON; FAN CHEVRON NOZZLE; PROPULSION AIRFRAME AEROACOUSTICS; SECONDARY FLOW;

ACOUSTIC NOISE; ACOUSTICS; COMPUTATIONAL METHODS; FLOW OF FLUIDS; KINETIC ENERGY; NAVIER STOKES EQUATIONS;

NOZZLES;

EID: 33845742971     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

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