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Limit Cycle Flutter Analysis of a High-Aspect-Ratio Wing with an External Store
Abstract:
Limit cycle flutter analysis of a high-aspect-ratiowing with an external store is presented. The concentrated store mass iscombined into the governing equations which are obtained using the extendedHamilton’s principle. The high-aspect-ratio wing structural model, which alsoconsiders the in-plane bending motion, is used. Three possible nonlinearitiesare considered including structural nonlinearities, aerodynamic nonlinearities,and store nonlinearities. Time simulation and bifurcation diagrams areperformed to analysis systems with three nonlinearities.
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907-910
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April 2014
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© 2014 Trans Tech Publications Ltd. All Rights Reserved
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