After recalling the general principles of aeroelastic coupling with structural finite element analysis, the simplifying assumptions of static aeroelasticity are explained. The technique of load basis used in a general aircraft structural analysis program is discussed. This technique allows one to separate the big expensive computation of finite element resolutions and theoretical aerodynamic analysis from aeroelastic coupling and flight maneuver computation.
Trends in Aeroelastic Analysis of Combat Aircraft
1987
25 pages
Report
No indication
English
Aeroelastic and environment analysis technology vs development of modern combat aircraft
British Library Conference Proceedings | 1993
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