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Shock structure in a simple discrete velocity gas. (English) Zbl 0123.21102

Keywords:
fluid mechanics
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[1] Krook, Astrophys. J. 122 pp 488– (1955)
[2] E. P. Gross, inProceedings of the First International Symposium on Rarefied Gas Dynamics, edited by F. M. Devienne (Pergamon Press, Inc., New York, 1960).
[3] J. E. Broadwell, J. Fluid Mech. (to be published). · Zbl 0118.42401
[4] Since the mean free path was defined for a state in which the Ni’s were equal, it would perhaps be more rigorous to use state (b) as the reference state instead of (a). It is usual, however, to refer the shock thickness to {\(\lambda\)}a, and in the present case it seems justified to apply formally the equation {\(\lambda\)} = 3(1+22)Sn in state (a).
[5] Mott-Smith, Phys. Rev. 82 pp 885– (1951)
[6] P. Glansdorff, inProceedings of the Second International Symposium on Rarefied Gas Dynamics, edited by L. Talbot (Academic Press, Inc., New York, 1961).
[7] N. Rott and C. G. Whittenbury, Douglas Aircraft Company Report SM-38524 (1961).
[8] Ziering, Phys. Fluids 4 pp 975– (1961)
[9] Glansdorff, Phys. Fluids 5 pp 371– (1962)
[10] Liepmann, Phys. Fluids 5 pp 1313– (1962)
[11] Whitham, Comm. Pure and Appl. Math. XII pp 113– (1959)
[12] Vincenti, J. Fluid Mech. 6 pp 481– (1959)
[13] Moore, J. Aerospace Sci. 27 pp 117– (1960)
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