Trailing edge noise prediction based on a new acoustic formulation

8th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Casper, J ^a   Farassat, F ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FORMULATIONS; AIRFOIL SURFACES; ANALYTICAL RESULTS; FFOWCS WILLIAMS-HAWKINGS EQUATION; LOW-MACH-NUMBER FLOW; ROTATING REFERENCE FRAME; SURFACE PRESSURE DISTRIBUTION; TRAILING EDGE NOISE;

AEROACOUSTICS; AIRFOILS; FORECASTING; LOADING; MACH NUMBER;

ACOUSTIC NOISE;

EID: 84896862177     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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