Stagnation region solutions of the full viscous shock-layer equations

The range of validity of the full viscous shock-layer equations was investigated. Numerical solutions were obtained by combining an implicit finite-difference scheme with a relaxation technique for determining the bow shock shape, and results were compared with experimental stagnation point data for...

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Veröffentlicht in:AIAA journal 1976-02, Vol.14 (2), p.274-276
Hauptverfasser: Srivastava, B.N., Werle, M.J., Davis, R.T.
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creator Srivastava, B.N.
Werle, M.J.
Davis, R.T.
description The range of validity of the full viscous shock-layer equations was investigated. Numerical solutions were obtained by combining an implicit finite-difference scheme with a relaxation technique for determining the bow shock shape, and results were compared with experimental stagnation point data for spherical nose shapes. The viscous shock-layer model was found to be in good agreement with experiment to very low Reynolds numbers. With the inclusion of shock and body slip, the full viscous shock-layer model is valid with shock Reynolds numbers as low as 20 to 30.
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title Stagnation region solutions of the full viscous shock-layer equations
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