An efficient and robust method for predicting helicopter rotor high-speed impulsive noise

34th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1996, Pages

  Brentner, Kenneth S ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE MEASUREMENT; AEROSPACE ENGINEERING; IMPULSE NOISE;

COMPUTATIONAL WORK; COMPUTER RESOURCES; FAR FIELD APPROXIMATION; HIGH-SPEED IMPULSIVE NOISE; NOISE COMPUTATIONS; NOISE PREDICTIONS; SURFACE INTEGRALS; TIME DERIVATIVE;

FORECASTING;

EID: 85088056856     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-151     Document Type: Conference Paper

References (24)

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