Abstract
AbstractNumerical solutions are presented for the problem of minimum weight design of a thin one‐dimensiona simply‐supported, solid panel in compression with one side exposed to a parallel high supersonic air flow. The flutter speed is held fixed, and a minimum thickness constraint is imposed. In addition, a multiplier technique is incorporated into the discrete variable minimization process to improve the convergence speed.
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Schedule a callMore From: International journal for numerical methods in engineering
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