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Viscous sublayer in the neighborhood of a corner point in supersonic flow past a cooled body

✍ Scribed by T. V. Konotop


Publisher
Springer
Year
1990
Tongue
English
Weight
349 KB
Volume
24
Category
Article
ISSN
0015-4628

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## Abstract A finite difference method for solving mixed initial and boundary value problems governed by hyperbolic partial differential equations is described. The method has been developed specifically to calculate the flow field associated with any arbitrary two‐dimensional or axi‐symmetric body