Spray characteristics of jet–swirl nozzles for thrust chamber injector

Author:

Hamid Ahmad Hussein Abdul,Atan Rahim

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference8 articles.

1. Numerical prediction of air core diameter, coefficient of discharge and spray cone angle of a swirl spray pressure nozzle;Datta;International Journal of Heat and Fluid Flow,2000

2. R.L. Ewen, H.M. Evensen, Liquid rocket engine self-cooled combustion chambers, in: NASA Space Vehicle Design Criteria, NASA SP-8124, 1977

3. D. Haeseler, C. Mäding, V. Rubinski, V. Kosmatcheva, V. Berezhnoy, N. Bratukhin, Injector issues with different propellant combinations, in: 5th International Symposium on Liquid Space Propulsion, Chattanooga, TN, USA, 2003

4. A numerical and experimental investigation on the coefficients of discharge and the spray cone angle of a solid cone swirl nozzle;Halder;Experimental Thermal and Fluid Science,2003

5. D. Jones, Reusable rocket propulsion for space tourism vehicles, AIAA 2004-3742, 2004

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