Integration of hypersonic viscous shock layer equations by a successive approximation method

DOI10.1016/0041-5553(78)90015-0zbMath0503.76055OpenAlexW1976543154MaRDI QIDQ3970038

I. G. Brykina

Publication date: 1978

Published in: USSR Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0041-5553(78)90015-0

zbMATH Keywords

convergencesuccessive approximation methodpressurefrictionheat transfervelocitycritical linetwo-dimensionalablationenthalpyviscous shock layer equationsCheng's two-layer modelflow past sphere, paraboloid and hyperboloidmoderately small Reynolds numbersperfect gas past plane and axisymmetric bodies

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Basic methods in fluid mechanics (76M99)

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