Numerical solutions of reactive fluid flows during postignition transients in hybrid rocket systems-Reference-Cited by-同舟云学术

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Numerical solutions of reactive fluid flows during postignition transients in hybrid rocket systems

Published:1972-04 Issue:2 Volume:9 Page:167-193
ISSN:0021-9991
Container-title:Journal of Computational Physics
language:en
Short-container-title:Journal of Computational Physics

Author:

Hung W.S.Y,Chen C.S,Haviland J.K

Publisher

Elsevier BV

Subject

Computer Science Applications,Physics and Astronomy (miscellaneous),Applied Mathematics,Computational Mathematics,Modeling and Simulation,Numerical Analysis

Reference32 articles.

1. Solid Fuel Combustion as Applied to Ramjets;Bartel,1946

2. Chemical Rocket Propulsion and Combustion Research;Penner,1962

3. Some Analytical Considerations of the Hybrid Rocket Combustion Problem;Fineman,1962

4. Introductory considerations on hybrid rocket combustion;Leon,1964

5. Regression Rate Mechanism of Nonmetallized Hybrid Fuel Systems;Smoot,1965

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A hybrid, non-split, stiff/RKC, solver for advection–diffusion–reaction equations and its application to low-Mach number combustion;Combustion Theory and Modelling;2019-04-05

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