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Explosive Induced Shock Waves. Part I. Plane Shock Waves
1.Walsh, Shreffler, and Willig, J. Appl. Phys. 24, 349 (1953).
1.J. M. Walsh and R. H. Christian, Phys. Rev. 97, 1544 (1955).
1.Pack, Evans, and James, Proc. Phys. Soc. (London) 60, 1 (1948).
2.W. E. Drummond, J. Appl. Phys. 28, 76 (1957). (Hereafter referred to as A.)
3.See R. Courant and K. O. Friedrichs, Supersonic Flow and Shock Waves (Interscience Publishers, Inc., New York, 1948).
4.For a discussion of this, see J. von Neumann, Office of Scientific Research and Development Report 549, April 1, 1942.
5.G. I. Taylor, Proc. Roy. Soc. (London) A200, 235 (1950).
6.Primes attached to variables; i.e., u, l, p, etc., refer to values of these quantities in the metal. Primes attached to capital letters refer to points or lines in the hodograph plane.
7.K. O. Friedrichs, Communs. Pure Appl. Math. 1, No. 3, p. 211.
8.J. M. Walsh and R. H. Christian, Phys. Rev. 97, 1544 (1955) and private communication.
9.R. E. Duff and E. Houston, J. Chem. Phys. 23, 1268 (1955).
10.This can be used only for high pressures.
11.C. M. Ablow (private communication). I would like to thank Dr. Ablow for communicating his results to me in advance of publication.
12.The term “effective” thickness is used here in an intuitive sense and no precise definition is implied. The “corrections” due to the method of detonation should be understood in this sense.
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