Solution of inverse problem of the theory of nonsteady solid propellant combustion under the pressure drop in rocket engine-Reference-Cited by-同舟云学术

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Solution of inverse problem of the theory of nonsteady solid propellant combustion under the pressure drop in rocket engine

Published:2018 Issue: Volume: Page:
ISSN:0094-243X
Container-title:AIP Conference Proceedings
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Author:

Novozhilov Boris,Marshakov Vladimir,Novozhilov Vasily

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Link

http://aip.scitation.org/doi/pdf/10.1063/1.5081588

Reference11 articles.

1. V.N. Marshakov, Dr. Phys. Math. Sci. Thesis (Inst. Chem. Phys. USSR Acad. Sci., Moscow, 1986).

2. Ya.B. Zeldovich, J. Exp. Theor. Phys. 12, 498 (1942).

3. B.V. Novozhilov, Nonsteady Combustion of Solid Rocket Fuels (Nauka, Moscow, 1973).

4. Combustion of a propellant and its extinction upon rapid depressurization: A comparison of theory and experiment

5. A.N. Tikhonov and V.Ya. Arsenin, Methods for Solving Ill-Posed Problems (Nauka, Moscow, 1979).

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