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- W1993638863 abstract "A finite element-boundary element compling procedure is applied to the computation of a transonic, compressible full potential flow past an airfoil. We require the Kutta-Joukowski condition as continuity of the pressure field at the trailing edge, Under the assumption of subsonic flow at the trailing edge and using classical regularity results for the solutions of elliptic first order systems, we prove the Holder continuity of the velocity in a vicinity of the trailing edge and get a local representation formula for the velocity. The Kutta-Joukowski condition enforces that the so-called stress intensity factor in this representation vanishes. The numerical FEM-BEM coupling procedure is executed in spaces of finite element functions charaeterized by the linear side condition of vanishing approximate stress intensity factors. The lincar side condition is formulated in terms of the Maz ya functional for the stress intensity factor. Detailed numerical implementation and numerical results are presented." @default.
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- W1993638863 date "1999-08-01" @default.
- W1993638863 modified "2023-09-27" @default.
- W1993638863 title "On the Treatment of the Kutta-Joukowski Condition in Transonic Flow Computations" @default.
- W1993638863 doi "https://doi.org/10.1002/(sici)1521-4001(199908)79:8<507::aid-zamm507>3.0.co;2-b" @default.
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