Results 11 to 20 of about 13,320 (264)
Multiple exhaust nozzles for nuclear rocket engines [PDF]
3rd Annual Meeting, 1966 D. Vanica, E. Duke
+8 more sources
Comparison of two procedures for predicting rocket engine nozzle performance [PDF]
23rd Joint Propulsion Conference, 1987 Two nozzle performance prediction procedures which are based on the standardized JANNAF methodology are presented and compared for four rocket engine nozzles. The first procedure required operator intercedence to transfer data between the individual performance programs.
Ken Davidian
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Supersonic Flow Separation with Application to Rocket Engine Nozzles
Applied Mechanics Reviews, 2005 The past decade has seen a qualitative advancement of our understanding of physical phenomena involved in flow separation in supersonic nozzles; in particular, the problem of side loads due to asymmetrical pressure loads, which constitutes a major restraint in the design of nozzles for satellite launchers.
Barbro Muhammad-Klingmann +2 more
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Acoustical Measurements of Static Tests of Clustered and Single-Nozzled Rocket Engines [PDF]
The Journal of the Acoustical Society of America, 1964 The predictions of the acoustic effects of the static firing of large rocket engines have usually been based upon such engine parameters as specific impulse, nozzle diameter, etc. However, the recent development of large clusters of smaller engines have introduced a new possible variant.
Richard N. Tedrick
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Fluid–structure interaction study of the start-up of a rocket engine nozzle [PDF]
Computers & Fluids, 2010 The aim of this paper is to analyze the aeroelastic processes developed during the starting phase of a rocket engine via a coupling fluid/structure code. This analysis gives a better understanding of the behavior of the structure as the shock waves propagate inside the engine nozzle.
Garelli, Luciano +2 more
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Case Studies in Thermal Engineering, 2021 This study aims to scrutinize the mathematical formulations of hybrid nanoliquid filled with thermal radiation, Cattaneo-Christov heat theory and melting phenomenon in a nozzle of rocket engine that includes hybrid nanoparticles (CoFe2O4,CdTe,TiO2,Cu&CuO)
Hassan Waqas +4 more
doaj +2 more sources
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроениеOne of the ways to increase the efficiency of a rocket engine chamber is to ensure the fixed nozzle operation in the design mode over the entire range of altitudes (ambient pressure) of engine operation.
A. A. Kirshina +2 more
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Transonic Flow Field Analysis of a Minimum Nozzle Length Rocket Engine [PDF]
INCAS BulletinThe aim of this paper is to develop a profile of axisymmetric minimum length nozzle giving a uniform and parallel flow at the exit section. The study is done at high temperature, lower than the dissociation threshold of the molecules.
Omar ABADA, Hakim KBAB, Sidali HAIF
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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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CFD Analysis of De Laval Nozzle of a Hybrid Rocket Engine [PDF]
E3S Web of Conferences: The study gives a general overview of the CFD-simulated gas flow via the nozzle of a De Laval rocket engine. In CFD software, the mesh is generated using the nozzle’s geometry.
Ahmad Mohamed Tarmizi +6 more
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