Panel flutter optimizationβa refined fin
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Terrence A. Weisshaar
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Article
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1976
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John Wiley and Sons
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English
β 862 KB
## Abstract This paper presents the results of an aeroelastic optimization study. In this study the weight of a large aspect ratio panel immersed in high Mach number supersonic flow is minimized subject to the requirement that a critical aeroelastic parameter for flutter be held within specified li