Nonlinear Aeroelastic Analysis of a High-Aspect-Ratio Wing with Large Deflection Effects
نویسندگان
چکیده
منابع مشابه
modal and aeroelastic analysis of a high-aspect-ratio wing with large deflection capability
this paper describes a modified structural dynamics model for aeroelastic analysis of high-aspect-ratio wings undergoing large deformation behavior. to gain this aim, a moderate deflection beam model is modified with some important large deflection terms and then coupled with a state space unsteady aerodynamics model. finite element method is used to discretize the equations of motion. a dynami...
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ژورنال
عنوان ژورنال: International Journal of Aeronautical and Space Sciences
سال: 2006
ISSN: 2093-274X
DOI: 10.5139/ijass.2006.7.1.099