论文信息 - Extensions to the Minimum-State Aeroelastic Modeling Method

Extensions to the Minimum-State Aeroelastic Modeling Method

Simple and direct expressions for the evaluation of the nonelementary part of the Kernel function of the integral equation relating the pressure and the normal wash distribution in supersonic nonstationary flow has been presented. It has been shown that the solutions presented are related to the same functional solutions of the subsonic Kernel. The expressions presented here can provide the basis for the development of numerical nonstationary interfering lifting surface methods. References

Mordechay Karpel | M. Karpel

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