Novel boundary integral formulation for blade-vortex interaction aerodynamics of helicopter rotors

AIAA Journal

Volumn 45, Issue 6, 2007, Pages 1169-1176

  Gennaretti, Massimo ^a,b   Bernardini, Giovanni ^a  

^a ROMA TRE UNIVERSITY   (Italy)

^b Mechanical and Industrial Eng Dept   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

BLADE PRESSURE FIELDS; BOUNDARY INTEGRAL FORMULATION; FREE WAKE EVOLUTION; VORTEX INTERACTION;

ACOUSTIC FIELDS; AERODYNAMICS; ASYMPTOTIC STABILITY; WAKES; WIND TUNNELS;

HELICOPTER ROTORS;

EID: 34347222855     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.18383     Document Type: Article

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