An effective transonic inverse design method for aeroelastic wing 基于控制理论方法的跨声速弹性机翼反设计方法研究
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An analysis method of loads on aircraft elastic wing with its real deformation considered 方程的弹性机翼载荷分析方法研究
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The research of this dissertation is focused on how to solve the 3 - dimensional compressible navier - stokes equations by the implicit finite difference algorithm and to simulate numerically the unsteady subsonic and transonic viscous flows around rigid and elastic wings . on the base of them the aeroelastic characterictics of an elastic wing have been studied 本文的主要工作是用隐式有限差分法求解三维非定常紊流n - s方程组，数值模拟刚性机翼及弹性机翼的亚、跨、超音速定常及非定常粘性绕流，并在此基础上研究了弹性机翼的气动弹性问题。
