High-order compact difference scheme applied to double-delta wing vortical flows

Journal of Aircraft

Volumn 41, Issue 4, 2004, Pages 953-957

  Arasawa, Tomoyuki ^a,c   Fujii, Kozo ^b,d   Miyaji, Koji ^a,c  

^a YOKOHAMA NATIONAL UNIVERSITY   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c Department of Environment Sciences ^*  (Japan)

^d JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVES; APPROXIMATION THEORY; BOUNDARY CONDITIONS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; DRAG; NAVIER STOKES EQUATIONS; PROBLEM SOLVING; SUPERSONIC AERODYNAMICS; TRANSONIC AERODYNAMICS; VORTEX FLOW;

DOUBLE-DELTA WINGS; GRID RESOLUTION; HIGH-SPEED AIRCRAFTS; VORTICAL FLOWS;

DELTA WING AIRCRAFT;

EID: 4344609105     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.3799     Document Type: Article

References (10)

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