Results 21 to 30 of about 50,563 (351)

Numerical Investigation on the Thermal Behaviour of a LOx/LCH4 Demonstrator Cooling System

open access: yesAerospace, 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
doaj   +1 more source

Progress in Regenerative Cooling and Coking Carbon Accumulation of High-Density Heat-Absorbing Hydrocarbon Fuels [PDF]

open access: yesHangkong bingqi
Hypersonic scramjet engines encounter extreme thermal loading conditions during sustained operation. Regenerative cooling has emerged as a cost-efficient and thermodynamically viable strategy for extreme thermal protection in hypersonic propulsion ...
Ma Zhengzheng, Mao Qian, Cheng Yifan, Shi Baolu, Wang Ningfei
doaj   +1 more source

Comparison and Evaluation of Transport Property Prediction Performance of Supercritical Hydrocarbon Aviation Fuels and Their Pyrolyzed Products via Endothermic Reactions

open access: yesEnergies, 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
doaj   +1 more source

Analysis and multi-response optimization of two dew point cooler configurations using the desirability function approach

open access: yesEnergy Reports, 2021
Due to climate change and hot summers in most of Algeria’s regions, air conditioning has become a thorny issue, resulting in excessive energy consumption.
A.F. Boudjabi   +6 more
doaj   +1 more source

Energy saving potential of a counter-flow regenerative evaporative cooler for various climates of China: Experiment-based evaluation [PDF]

open access: yes, 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
core   +1 more source

Influence of curvature in regenerative cooling system of rocket engine [PDF]

open access: yesProgress 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.
openaire   +2 more sources

Numerical framework of hybrid nanofluid over two horizontal parallel plates with non-linear thermal radiation

open access: yesInternational Journal of Thermofluids, 2023
Significance of study: High combustion temperatures necessitate appropriate cooling systems in the combustion process. Regenerative cooling is used in the majority of chambers in liquid propellant engines.
Umar Farooq   +8 more
doaj   +1 more source

Experimental study of a counter-flow regenerative evaporative cooler [PDF]

open access: yes, 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
core   +1 more source

Preliminary Design and Simulation of a Thermal Management System with Integrated Secondary Power Generation Capability for a Mach 8 Aircraft Concept Exploiting Liquid Hydrogen

open access: yesAerospace, 2023
This paper introduces the concept of a thermal management system (TMS) with integrated on-board power generation capabilities for a Mach 8 hypersonic aircraft powered by liquid hydrogen (LH2).
Davide Ferretto, Nicole Viola
doaj   +1 more source

Effects of thermal and pressure loads on structural deformation of liquid oxygen/methane engine combustion chamber

open access: yesJournal of Thermal Science and Technology, 2020
To investigate the influences of thermal and pressure loads on the structural deformation of the Liquid Oxygen/Methane rocket engine combustion chamber, a complete thermo-structural analysis scheme including fluid-thermal analysis and structural finite ...
Di LIU   +4 more
doaj   +1 more source

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