Results 81 to 90 of about 2,824 (228)
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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Combustion Instability of Liquid Rocket Engines [PDF]
, 2004 D. K. Sung, Hwanil Huh, Chae-Hoon Sohn
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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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Journal of Aerospace Technology and Management, 2011 This study presents the results of the investigation of a cooling method widely used in the combustion chambers, which is called cooling film, and it is applied to a liquid rocket engine that uses as propellants liquid oxygen and kerosene.
Luís Antonio Silva
doaj
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроениеIn this paper, various configurations of jet nozzles are analyzed, as well as their design. The effects of the inlet chamfer of jet nozzles on their flow rate and range are considered.
Yu. I. Ageenko, A. S. Bubnova
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Combustion Characteristics of Fuel-rich Gas Generator with Impinging Injector for a Liquid Rocket Engine [PDF]
, 2005 Yeoung-Min Han +5 more
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Radial Turbine Preliminary Aerodynamic Design Optimization for Expander Cycle Liquid Rocket Engine [PDF]
, 2006 Yolanda Mack +6 more
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Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроениеThe paper presents the results of simulation of spray and combustion processes in the liquid-propellant rocket engine chamber using the z77 reduced kinetic mechanism of chemical reactions and a hybrid method for determining spray parameters of a swirl ...
M. N. Senchev +4 more
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Development of Combustion Test Facility for Liquid Rocket Engine [PDF]
, 2006 Dong-Hwan Kim +2 more
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Rotordynamic Analysis of a High Thrust Liquid Rocket Engine Turbopump [PDF]
, 2008 Seong-Min Jeon +3 more
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