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The Formation and Properties of Liquid Sheets Suitable for Use in Rocket Engine Injectors [PDF]
Formation and properties of liquid sheets suitable for use in rocket engine ...
Riebling, R. W.
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Mehran University Research Journal of Engineering and Technology, 2019 Optimum characteristic length of the combustion chamber of liquid rocket engine is very important to get higher energy from the liquid propellants. Characteristic length is defined by the time required for complete burning of fuel.
Tajwali Khan, Ihtzaz Qamar
doaj
International Journal of Aerospace Engineering, 2012 Pressure and temperature of the liquid rocket thrust chambers into which propellants are injected have been in an ascending trajectory to gain higher specific impulse.
Bruce Chehroudi
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The prediction of the nonlinear behavior of unstable liquid rockets [PDF]
Analytical technique for solving nonlinear combustion problems associated with liquid propellant rocket ...
Powell, E. A., Zinn, B. T.
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Combustion Instability of Liquid Rocket Engines [PDF]
, 2004 D. K. Sung, Hwanil Huh, Chae-Hoon Sohn
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The effect of mixing, radiation, and finite rate combustion upon the flow field and surroundings of the exhaust plumes of rocket engines burning RP1 /kerosene/ and liquid oxygen [PDF]
Shear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engine exhaust plume ...
Edelman, R., Fortune, O.
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Transient Heat Transfer and Structural Analyses for the Turbopump Turbine of a Liquid Rocket Engine [PDF]
, 2004 Jae-Han Yoo +5 more
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Summary of literature survey of hypergolic ignition spike phenomena, phase I Final report, Apr. 8 - Dec. 31, 1965 [PDF]
Summary of industry survey and literature search of ignition spike phenomena in low thrust, hypergolic, liquid bipropellant rocket ...
Christos, T., Perlee, H. E.
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Optimal Design of Fuel-Rich Gas Generator for Liquid Rocket Engine [PDF]
, 2004 Sun-Tak Kwon, Changjin Lee
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