Effect of blade-tip shape on high-speed rotor noise

14th Applied Aerodynamics Conference

Volumn , Issue , 1996, Pages 80-89

  Aoyama, Takashi ^a   Aokl, Makoto ^b   Kondo, Natsuki ^b   Saito, Shigeru ^a   Kawachi, Keiji ^c  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Advanced Technology Institute of Commuter helicopter Ltd   (Japan)

^c UNIVERSITY OF TOKYO   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTICS; AERODYNAMICS; HELICOPTER ROTORS; ITERATIVE METHODS; SHOCK WAVES;

ACOUSTIC PRESSURES; ACOUSTIC SOURCES; HIGH-SPEED ROTORS; KIRCHHOFF'S EQUATION; MOVING SURFACES; NEAR-FIELD ACOUSTICS; NEWTON ITERATIVE METHODS; SOURCE PRESSURE;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84964238149     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)

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