Nonlinear response functions of the burning rate of ballistite powders

Author:

Zenin A. A.,Finjakov S. V.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference33 articles.

1. A. A. Zenin and S. V. Finjakov, “Burning-rate response functions of nitramine-based propellants and HMX from microthermocouple data measurements,” Combust., Expl., Shock Waves, 36, No. 1, 10–20 (2000).

2. E. W. Price, “Experimental observations of combustion instability,” in: K. K. Kuo and M. Summerfield (eds.), Progress in Astronautics and Aeronautics, Vol. 90: Fundamentals of Solid-Propellant Combustion, AIAA, New York (1984), pp. 733–790.

3. J. S. T’ien, “Theoretical analysis of combustion instability,” ibid., pp. 791–840.

4. F. E. C. Culick and V. Yang, “Prediction of the stability of unsteady motions in solid-propellant rocket motors,” in: L. De Luca, E. W. Price, and M. Summerfield (eds.), Progress in Astronautics and Aeronautics, Vol. 143: Combustion Stability of Solid Propellants, AIAA, Washington (1992), pp. 719–780.

5. B. V. Novozhilov, M. Kohno, H. Maruizumi, and T. Shimara, “Solid propellant burning rate response functions of higher orders,” The Inst. of Space and Astronaut. Sci. Report No. 661, Kanagava (1996); http://ci.nii.ac.jp/naid/110000029174/en/ .

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1. Nonlinear response functions of the burning rate of RDX and HMX;Combustion, Explosion, and Shock Waves;2013-09

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