Comparison of static and dynamic fluid-structure interaction solutions in the case of a highly flexible modern transport aircraft wing

Aerospace Science and Technology

Volumn 7, Issue 2, 2003, Pages 121-133

  Girodroux Lavigne, P ^e   Grisval, J P ^e   Guillemot, S ^c   Henshaw, M ^b   Karlsson, A ^f   Selmin, V ^a   Smith, J ^d   Teupootahiti, E ^c   Winzell, B ^f  

^a ALENIA SPAZIO   (Italy)

^b BAE SYSTEMS   (United Kingdom)

^c DASSAULT AVIATION   (France)

^d Aeronautical Research Institute of Sweden   (Sweden)

^e ONERA   (France)

^f SAAB AB   (Sweden)

Author keywords

Dynamic aeroelasticity; Fluid structure coupling; Flutter prediction; Numerical simulation; Static aeroelasticity; Transonic flows

Indexed keywords

COMPUTER SIMULATION; FLUID STRUCTURE INTERACTION; FLUTTER (AERODYNAMICS); TIME DOMAIN ANALYSIS; WINGS;

FLUID STRUCTURE COUPLING; FLUTTER PREDICTION;

TRANSONIC AERODYNAMICS;

EID: 0346093756     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(02)00007-X     Document Type: Article

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