Results 191 to 200 of about 29,920 (238)
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Combustion in Liquid-Fuel Rocket Motors
Aeronautical Quarterly, 1959SummaryThe paper provides a simplified picture of the processes occurring in liquid bi-propellant rocket motors. Droplet vaporisation, chemical reaction, and drag between gas and droplet are considered for a one-dimensional model. Quantitative theoretical results are presented for the variation of droplet size, droplet velocity, gas temperature and gas
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Resonant Combustion in Rockets
Scientific American, 1968J. George Sotter, Gary A. Flandro
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The Sampling of Rocket Combustion Gases
The Journal of the Royal Aeronautical Society, 1964Summary:—In the past, attempts have been made to evaluate injectors for rocket engine combustion chambers by the use of water analogy rigs and model combustion systems that simulated the injection and combustion phase change occurring in the actual engine.
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Boron Combustion Characteristics in Ducted Rockets
Combustion Science and Technology, 1972Abstract A test program was performed with the objective of experimentally investigating the boron reaction characteristics in a ducted rocket by systematically varying the primary chamber conditions. In order to vary the primary chamber conditions a test device was used which burned boron powder and gaseous propellants (hydrogen or carbon monoxide ...
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Bifurcation of liquid rocket combustion
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998Renat Doulatov +2 more
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Studies of staged combustion rocket motor combustion characteristics
7th Propulsion Joint Specialist Conference, 1971H. DYER, C. WARNER
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Combustion Instability in Gas Rockets
AIAA Journal, 1965C. T. BOWMAN, I. GLASSMAN, L. CROCCO
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Transient combustion in hybrid rockets
31st Joint Propulsion Conference and Exhibit, 1995M Karabeyoglu, D Altman, D Bershader
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Combustion Studies in Rocket Motors
Journal of the American Rocket Society, 1953KURT BERMAN, SAMUEL H. CHENEY
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