A scaling method for combustion stability rating of coaxial gas-liquid injectors in a subscale chamber-Reference-Cited by-同舟云学术

A scaling method for combustion stability rating of coaxial gas-liquid injectors in a subscale chamber

Published:2012-11 Issue:11 Volume:26 Page:3691-3699
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Sohn Chae Hoon,Kim Young Jun,Kim Young-Mog,Pikalov Valery P.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://link.springer.com/content/pdf/10.1007/s12206-012-0843-3.pdf

Reference18 articles.

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4. D. K. Huzel and D. H. Huang, Modern engineering for design of liquid-propellant rocket, Vol. 147, Progress in Astronautics and Aeronautics, AIAA, Washington, DC (1992) 35.

5. G. P. Sutton, History of liquid-propellant rocket engines in Russia, formerly the Soviet Union, Journal of Propulsion and Power 19 (2003) 1008–1037.

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