Limit Cycle Flutter Analysis of a High-Aspect-Ratio Wing with an External Store

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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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Periodical:

Advanced Materials Research (Volumes 912-914)

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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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