Occurrence conditions for unsteady combustions in shock-induced combustions around spherical projectiles

Author:

MAEDA Shinichi1,YOSHIKI Isshu1,KANNO Shoichiro1,TOMITA Keita2,OBARA Tetsuro1

Affiliation:

1. Graduate School of Science and Engineering, Saitama University

2. Faculty of Engineering, Saitama University

Publisher

Japan Society of Mechanical Engineers

Reference26 articles.

1. Alpert, R.L. and Toong, T.Y., Periodicity in exothermic hypersonic flows about blunt projectiles, Astronautica Acta, Vol.17 (1972), pp.539-560.

2. Dudebout, R., Sislian, J.P. and Oppitz, R., Numerical simulation of hypersonic shock-induced combustion ramjets, Journal of Propulsion and Power, Vol.14, No.6 (1998), pp.869-879.

3. Gordon, S. and McBride, B.J., Computer program for calculation of complex chemical equilibrium compositions and applications, NASA Reference Publication, No.1311 (1994).

4. Higgins, A.J. and Bruckner, A.P., Experimental investigation of detonation initiation by hypervelocity blunt projectiles., AIAA paper, 96-0342 (1996).

5. Iwata, K., Nakaya, S. and Tsue, M., Numerical investigation of the effects of nonuniform premixing on shock-induced combustion, AIAA Journal, Vol.54, No.5 (2016), pp.1682-1692.

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