An efficient and robust method for computing quadrupole noise

Journal of the American Helicopter Society

Volumn 42, Issue 2, 1997, Pages 172-181

  Brentner, Kenneth S ^a   Holland, Peter C ^b,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b GEORGE WASHINGTON UNIVERSITY   (United States)

^c ROLLS ROYCE CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC INTENSITY; ACOUSTIC NOISE; APPROXIMATION THEORY; COMPUTATIONAL METHODS; INTEGRATION; SUBSONIC AERODYNAMICS;

EULER PREDICTIONS; FAR FIELD APPROXIMATION; FFOWCS WILLIAMS-HAWKINGS QUADRUPOLE NOISE; MACH NUMBER; ROTOR BLADES;

HELICOPTER ROTORS;

EID: 0031122221     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/jahs.42.172     Document Type: Article

References (20)

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