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The Boundary Layer Equations of Compressible Flow. Separation
Author(s) -
Meksyn D.
Publication year - 1958
Publication title -
zamm ‐ journal of applied mathematics and mechanics / zeitschrift für angewandte mathematik und mechanik
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.449
H-Index - 51
eISSN - 1521-4001
pISSN - 0044-2267
DOI - 10.1002/zamm.19580380907
Subject(s) - boundary layer , compressibility , compressible flow , blasius boundary layer , flow (mathematics) , mechanics , flow separation , shock wave , prandtl number , shock (circulatory) , physics , mathematics , mathematical analysis , classical mechanics , medicine , heat transfer
The Equations of Motion, Continuity and Energy of compressible boundary layer are reduced to two equations which, in the case when Prandtl numer ∼ is equal to unity and ∼ T, are reduced to one equation identical with the equation for incompressible flow. It is applied to the case of flow past a plane with separation induced by a shock wave. An improved method of integration in indicated.