CFD validation study for a high-lift configuration of a civil aircraft model

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2007, Pages 474-493

  Murayama, Mitsuhiro ^a,c,d   Yokokawa, Yuzuru ^a,c,d   Yamamoto, Kazuomi ^a,c,d   Ueda, Yoshine ^b,e  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Tokyo Business Service Co Ltd   (Japan)

^c Aviation Program Group   (Japan)

^d AIAA   (United States)

^e NONE   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT MODELS; BOUNDARY LAYERS; THREE DIMENSIONAL COMPUTER GRAPHICS;

MESH METHOD; NACELLE-PYLON TESTED; REALISTIC AIRCRAFT; THREE-DIMENSIONAL FLOW COMPUTATIONS;

COMPUTATIONAL FLUID DYNAMICS;

EID: 35648987627     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-3924     Document Type: Conference Paper

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