Quarterly of Applied Mathematics

Quarterly of Applied Mathematics

Online ISSN 1552-4485; Print ISSN 0033-569X



On supersonic flow behind a curved shock

Author: R. E. Meyer
Journal: Quart. Appl. Math. 14 (1957), 433-436
MSC: Primary 76.0X
DOI: https://doi.org/10.1090/qam/83327
MathSciNet review: 83327
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References [Enhancements On Off] (What's this?)

  • [1] J. J. Mahony, A critique of shock-expansion theory, J. Aeronaut. Sci. 22, 673-680 (1955) MR 0072636
  • [2] J. J. Mahony, The flow around a supersonic aerofoil, Aero. Res. Lab. Melbourne Note A 147-1955.
  • [3] P. M. Stocker, Hypersonic flow: part I, Armament Research & Dev. Establ. (Ft. Halstead) Rep. (B) 22/55, 1955.
  • [4] L. Howarth (editor), Modern developments in fluid dynamics: high speed flow, Oxford University Press, 1953. MR 0059718
  • [5] R. Courant and K. O. Friedrichs, Supersonic flow and shock waves, Interscience, N.Y., 1948. MR 0029615
  • [6] R. E. Meyer, Focusing effects in two-dimensional supersonic flow, Phil. Trans. Roy Soc. A242, 153-171 (1949). MR 0033677

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DOI: https://doi.org/10.1090/qam/83327
Article copyright: © Copyright 1957 American Mathematical Society

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