Motion of an explosive-induced plane shock wave-Reference-Cited by-同舟云学术

Motion of an explosive-induced plane shock wave

Published:1974 Issue:1 Volume:32 Page:71-84
ISSN:0033-569X
Container-title:Quarterly of Applied Mathematics
language:en
Short-container-title:Quart. Appl. Math.

Author:

Fickett W.

Abstract

A plane, unsupported, Chapman-Jouguet detonation in a condensed explosive drives a decelerating shock into a semi-infinite inert of lower shock impedance. A previously reported exact solution for a portion of this one-dimensional time-dependent problem is extended to the entire flow field, and some numerical results are given. The solution has the form of a small set of first-order ordinary differential equations for the shock, and a similar set for each particle path.

Publisher

American Mathematical Society (AMS)

Subject

Applied Mathematics

Link

http://www.ams.org/qam/1974-32-01/S0033-569X-1974-99688-8/S0033-569X-1974-99688-8.pdf

Reference9 articles.

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2. W. E. Drummond, Explosive induced shock waves: Part 1, plane shock waves, J. Appl. Phys. 28, 1437–41 (1957)

3. V. N. Kondratev, I. V. Nemchinov, and B. D. Khristoforov, O zatukhanii v tverdom tele ploskikh udarnykh voln, vyzvannykh vzryvom (On the attenuation in a solid of a plane shock wave generated by explosive), Zh. Prikl. Mekh. Tekh. Fiz. 4, 61–65 (1968)

4. J. M. Walsh, Shock attenuation for an arbitrary impluse, General Atomic Division of General Dynamics Corp. Report GAMD-2341, June 19, 1961

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