CFD computations of NAL experimental airplane with rocket booster using overset unstructured grids

International Journal for Numerical Methods in Fluids

Volumn 48, Issue 8, 2005, Pages 801-818

  Togashi, Fumiya ^a   Fujita, Takeshi ^a   Ito, Yasushi ^a   Nakahashi, Kazuhiro ^a   Makino, Yoshikazu ^b  

^a TOHOKU UNIVERSITY   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

CFD; Experimental airplane; NAL; Overset method; Separation; Unstructured mesh

Indexed keywords

AIRCRAFT FUELING; BOOSTERS (ROCKET); COMPUTER SIMULATION; FUSELAGES; SUPERSONIC AERODYNAMICS;

AERODYNAMIC PERFORMANCE; ASCENT FLIGHT; BOOSTER MESHES; EULER EQUATIONS;

COMPUTATIONAL FLUID DYNAMICS;

COMPUTATIONAL FLUID DYNAMICS;

EID: 21544454109     PISSN: 02712091     EISSN: None     Source Type: Journal    
DOI: 10.1002/fld.940     Document Type: Article

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