Results 31 to 40 of about 1,571,082 (390)
Numerical Investigation on the Thermal Behaviour of a LOx/LCH4 Demonstrator Cooling System
Aerospace, 2021 Reliability of liquid rocket engines is strictly connected with the successful operation of cooling jackets, able to sustain the impressive operative conditions in terms of huge thermal and mechanical loads, generated in thrust chambers. Cryogenic fuels,
Daniele Ricci +2 more
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Energies, 2023 This study presents results of predicting the transport properties of hydrocarbon aviation fuels and their decomposed products after pyrolysis.
Sung-rok Hwang, Hyung Ju Lee
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Effect of Tube Geometry on Regenerative Cooling Performance [PDF]
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005 The flowfield characteristics in a rocket engine coolant channels are analyzed by use of a commercial CFD and multiphysics software developed by the CFD Research Corp. called CFD-ACE+. The channels are characterized by high Reynolds number flow, varying aspect ratio, varying curvature, asymmetric and symmetric heating.
D. Brian Landrum, Daniel K. Parris
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Experimental study of a counter-flow regenerative evaporative cooler [PDF]
, 2016 This paper aims to investigate the operational performance and impact factors of a counter-flow regenerative evaporative cooler (REC). This was undertaken through a dedicated experimental process.
Dong, Xuelin +3 more
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Energy saving potential of a counter-flow regenerative evaporative cooler for various climates of China: Experiment-based evaluation [PDF]
, 2017 © 2017 Recently there has been growing interest in regenerative evaporative coolers (REC), which can reduce the temperature of the supply air to below the wet-bulb of intake air and approach its dew-point.
Chen, Hongbing +4 more
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Energies, 2018 This paper presents a comparative study of the cross-flow regenerative heat and mass exchanger (HMX) and the conventional cross-flow HMX for indirect evaporative cooling (IEC) with numerical methods.
Yugang Wang, Xiang Huang, Li Li
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Aerospace, 2023 The cooling jackets of liquid rocket engines are composed of narrow passages surrounding the thrust chambers and ensure the reliable operation of the engine.
Daniele Ricci +3 more
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Influence of curvature in regenerative cooling system of rocket engine [PDF]
Progress in Propulsion Physics, 2009 Thermomechanical loads in rocket engines can be drastically reduced by a reliable cooling system. The regenerative cooling system uses propellants as coolant which §ows through milled cooling channels in the chamber walls. Due to centrifugal forces, dynamic secondary motions appearincooling-channelcurvatures,whichstronglymodify heattransfer.
Torres, Y., Stefanini, L., Suslov, D.
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Aerospace, 2023 An essential part of the design of a liquid rocket engine is the thermal analysis of the thrust chamber, which is a component whose operative life is limited by the maximum allowable wall temperature and heat flux.
Matteo Fagherazzi +3 more
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Improving the performance of LOX/kerosene upper stage rocket engines
Propulsion and Power Research, 2017 Improved liquid rocket engine cycles were proposed and analyzed via comparison with existing staged combustion and gas-generator cycles. The key features of the proposed cycles are regenerative cooling of thrust chamber by oxygen and subsequent use of ...
IgorN. Nikischenko +2 more
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