Results 81 to 90 of about 29,920 (238)
Numerical analysis of transient combustion response to acoustic oscillations in axisymmetric rocket motors [PDF]
, 1998 A numerical analysis of unsteady motions in solid rocket motors with a nozzle has been conducted. The formulation treats the complete conservation equations for the gas phase and the one-dimensional equations in the radial direction for the condensed
Culick, F. E. C., Roh, T. S.
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AN EXPERIMENTAL INVESTIGATION OF GASEOUS-FILM COOLING OF A ROCKET MOTOR [PDF]
Gaseous-film cooling of rocket combustion ...
Golladay, R. L., Lucas, J. G.
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Авіаційно-космічна техніка та технологіяThe subjects of this article are processes in the chamber of the pulse detonation propulsion system of the combined acceleration cycle (PSCA). The goal is to identify the most significant factors and study their influence on the defining characteristics ...
Olena Zolotko +4 more
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A study of two phase detonation as it relates to rocket motor combustion instability [PDF]
Two-phase detonation in rocket motor combustion instability - production of monodisperse ...
Dabora, E. K. +2 more
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Approximate theoretical performance evaluation for a diverging rocket [PDF]
, 1960 A simplified combustion model, which is motivated by available performance studies on the diverging rocket reactor, has been used as basis for an engine performance evaluation.
Eckel, E. F. +3 more
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Photographic investigation of propellant stream behavior in a firing rocket engine, volume I Technical summary report, 1 Aug. 1964 - 28 Feb. 1966 [PDF]
Photographic study to obtain injection and combustion patterns of F-1 rocket engine injector ...
Eulner, R. N. +2 more
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Injector-valve device Patent [PDF]
, 1965 Apparatus for cooling and injecting hypergolic propellants into combustion chamber of small rocket ...
Stein, S.
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Liquid hydrogen film cooled pressure transducers [PDF]
Liquid hydrogen film cooled pressure transducer for flush mounting in rocket combustion ...
Delmonte, J.
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Combustion chamber Patent [PDF]
, 1969 Regenerative cooling system for rocket combustion chamber using coolant tubes in convergent-divergent ...
Gregory, J. W.
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The problem of combustion instability in liquid rocket engines
Challenges and Issues of Modern ScienceThe purpose of this work is to carry out an overview on combustion instability in liquid propellant rocket engines, its classification, the main principles of occurrence as well as ways to prevent the phenomena while designing of the prospective engine.
Samir Vekilov +2 more
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