The analytical solution of an unsteady gas flow with shocks

DOI10.1007/S004190050108zbMath0892.76041OpenAlexW2027174448MaRDI QIDQ1372144

J. Ning

Publication date: 6 November 1997

Published in: Archive of Applied Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s004190050108

zbMATH Keywords

hypersonic flowsmethod of characteristicssupersonic flowsdetonation wavesimpulsive motion of piston

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Cites Work

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• Uniformly valid analytical solution to the problem of a decaying shock wave
• Approximate solution in gasdynamics
• Numerical integration of the gasdynamic equations
• Self-similar flows with uniform velocity gradient and their use in modelling the free expansion of polytropic gases
• Approximate and exact numerical computation of supersonic flow over an airfoil
• APPROXIMATE AND NUMERICAL SOLUTIONS OF A GASEOUS FLOW WITH SHOCKS
• Some exact solutions describing unsteady plane gas flows with shocks
• Formation and decay of shock waves

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