Simulation of aircraft response to control surface deflection using unstructured dynamic grids

20th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2002, Pages

  Murayama, Mitsuhiro ^a   Togashi, Fumiya ^a   Nakahashi, Kazuhiro ^a   Matsushima, Kisa ^a   Kato, Takuma ^a  

^a TOHOKU UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT CONTROL; CONTROL SURFACES; FLIGHT SIMULATORS; SUPERSONIC AIRCRAFT;

COMPUTATIONAL GRIDS; COMPUTATIONAL TECHNIQUE; CONTROL SURFACE DEFLECTION; CONTROL SURFACE RESPONSE; DYNAMIC MESH METHOD; NATIONAL AEROSPACE LABORATORIES; UNSTEADY SIMULATIONS; UNSTRUCTURED DYNAMIC GRIDS;

FIGHTER AIRCRAFT;

EID: 85067316665     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-2940     Document Type: Conference Paper

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