On the applicability of some approximate similitude laws in hypersonic aerodynamics

DOI10.1007/BF02324316zbMath0855.76036OpenAlexW2100145282MaRDI QIDQ1815105

Yanyan Li

Publication date: 11 December 1996

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf02324316

zbMATH Keywords

heat transferdrag coefficientfriction coefficientblunt bodiescomplete viscous shock layer equations

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Hypersonic flows (76K05)

Cites Work

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• Asymptotic solution of the Euler equations in the shock layer on a blunt body in nonuniform flow with gas injection from the body surface
• Heat transfer and drag of a body in a far supersonic wake
• Hypersonic three-dimensional viscous shock layer in a nonuniform gas flow in the neighborhood of the stagnation point

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