Flutter simulations of a T-tail configuration using non-linear aerodynamics

International Journal for Numerical Methods in Engineering

Volumn 72, Issue 13, 2007, Pages 1513-1523

  Arizono, Hitoshi ^a   Kheirandish, H R ^b   Nakamichi, J ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Research Center of Computational Mechanics Inc   (Japan)

Author keywords

Flutter; Non linear aerodynamics; T tail

Indexed keywords

ANGLE OF ATTACK; COMPUTER SIMULATION; MACH NUMBER; TRANSONIC FLOW;

T-TAIL CONFIGURATION;

FLUTTER (AERODYNAMICS);

ANGLE OF ATTACK; COMPUTER SIMULATION; FLUTTER (AERODYNAMICS); MACH NUMBER; TRANSONIC FLOW;

EID: 37249061202     PISSN: 00295981     EISSN: 10970207     Source Type: Journal    
DOI: 10.1002/nme.2047     Document Type: Article

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