The calculation of steady plane supersonic gas flows containing an arbitrarily large number of shocks

DOI10.1016/0021-9991(68)90022-3zbMath0172.53001OpenAlexW2078126722MaRDI QIDQ2531839

D. B. Taylor

Publication date: 1968

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-9991(68)90022-3

zbMATH Keywords

fluid mechanics

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The calculation of steady plane supersonic gas flows containing an arbitrarily large number of shocks

Cites Work

• On the convergence of characteristic finite-difference methods of high accuracy for quasi-linear hyperbolic equations
• Finite-difference calculations for hydrodanamic flows containing discontinuities
• The calculation of steady plane supersonic gas flows containing an arbitrarily large number of shocks
• On the solution of nonlinear hyperbolic differential equations by finite differences
• An Approximation to the Re-Entry Trajectory