Nonlinear aeroelastic computations of a wing/pylon/finned-store using parallel computing

AIAA Journal

Volumn 43, Issue 1, 2005, Pages 53-62

  Kim, Dong Hyun ^a,d   Park, Young Min ^b,e   Lee, In ^c,f   Kwon, Oh Joon ^c,f  

^a Gyeongsang National University   (South Korea)

^b Korea Aerospace Research Institute (KARI)   (South Korea)

^c Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^d Sch of Mech and Aerosp Eng   (South Korea)

^e Aerodynamics Division

^f Department of Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER OPERATING SYSTEMS; DATA TRANSFER; INTEGRAL EQUATIONS; OSCILLATIONS; PARALLEL PROCESSING SYSTEMS; SHOCK WAVES; SUPERSONIC FLOW; TRANSONIC FLOW; VIBRATION MEASUREMENT;

COMPUTER OPERATING SYSTEM - LINUX; FLUTTER BOUNDARY; NATURAL VIBRATION FREQUENCY; NONLINEAR AEROELASTIC ANALYSIS;

AERODYNAMICS;

EID: 12744274620     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.11011     Document Type: Article

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