The boundary layer nature of shock transition in a real fluid
Author:
G. S. S. Ludford
Journal:
Quart. Appl. Math. 10 (1952), 1-16
MSC:
Primary 76.1X
DOI:
https://doi.org/10.1090/qam/45533
MathSciNet review:
45533
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Additional Information
- L. M. Milne-Thomson, Theoretical Hydrodynamics, The Macmillan Company, New York, N. Y., 1950. 2nd ed. MR 0033660
H. Lamb, Lehrbuch der Hydrodynamik, Teubner, Leipzig, 1931, Appendix IV.
R. von Mises and K. O. Friedrichs, Fluid dynamics, Brown University Summer Session for Advanced Instruction and Research in Mechanics, 1941, pp. 140-143.
- R. Courant and K. O. Friedrichs, Supersonic Flow and Shock Waves, Interscience Publishers, Inc., New York, N. Y., 1948. MR 0029615
H. and B. S. Jeffreys, Mathematical physics, Cambridge University Press, Cambridge, 1946, Chapter 4.
- R. von Mises, On the thickness of a steady shock wave, J. Aeronaut. Sci. 17 (1950), 551–554. MR 37691
L. M. Milne-Thomson, Theoretical hydrodynamics, Macmillan and Co., London, 1950, p. 507.
H. Lamb, Lehrbuch der Hydrodynamik, Teubner, Leipzig, 1931, Appendix IV.
R. von Mises and K. O. Friedrichs, Fluid dynamics, Brown University Summer Session for Advanced Instruction and Research in Mechanics, 1941, pp. 140-143.
R. Courant and K. O. Friedrichs, Supersonic flow and shock waves, Interscience Publishers, Inc., New York, 1948, p. 16.
H. and B. S. Jeffreys, Mathematical physics, Cambridge University Press, Cambridge, 1946, Chapter 4.
R. von Mises, On the thickness of a steady shock wave, Journ. Aero. Sci. 17, 551-555 (1950).
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Article copyright:
© Copyright 1952
American Mathematical Society
