High fidelity multidisciplinary tool development for helicopter quieting

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2007, Pages 125-137

  Chen, C L ^a,g,h   Chen, Ya Chi ^a   Chen, Bing ^a   Jain, Rohit K ^b   Lund, Tom ^c   Zhao, Hongwu ^c   Wang, Z J ^d   Sun, Yuzhi ^d   Saberi, Hossein ^e   Shih, T H ^f  

^a Teledyne Scientific   (United States)

^b HYPERCOMP INC   (United States)

^c UNIVERSITY OF COLORADO   (United States)

^d IOWA STATE UNIVERSITY   (United States)

^e Advanced Rotorcraft Technology Inc   (United States)

^f OHIO AEROSPACE INSTITUTE   (United States)

^g Applied Computational Physics   (United States)

^h AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTICS; AERODYNAMICS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; ROBUST CONTROL;

AZIMUTHAL ANGLES; COMPUTATIONAL TOOL-WINDUS-HELI; ELASTIC BLADES; HELICOPTER BLADES; HELICOPTER QUIETING; STATE-OF-THE-ART NUMERICAL APPROACHES;

HELICOPTER ROTORS;

EID: 35649014269     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-3807     Document Type: Conference Paper

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