论文信息 - Large amplitude supersonic flutter of panels with ends elastically restrained against rotation

Large amplitude supersonic flutter of panels with ends elastically restrained against rotation

Abstract Nonlinear supersonic flutter of panels is studied for end conditions of simply supported, clamped and partial restrained against rotation by a unified approach. The effects of large deflection and inplane forces on flutter boundary is included. Based on convergence study an eight element solution is given for all the results presented.

G. Venkateswara Rao | G. Rao | K.Singa Rao | K. Rao

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