Heat transfer and flow structures of supercritical n-decane in a regenerative cooling channel loaded with non-uniform heat flux [PDF]
A harsh and complex thermal environment in the combustor threatens safe working of scramjets. In this study, heat transfer and flow structures of supercritical n-decane under 3 MPa in a regenerative cooling channel loaded with non-uniform heat flux ...
Jian Liu+4 more
doaj +3 more sources
Effect of Cooling Header on the Hydrocarbon Fuel Flow Distribution in a Regenerative Cooling Channel
Regenerative cooling technology is the most widely used cooling technology in liquid rocket engines, and flow distribution is very important for regenerative cooling heat transfer. In this work, the flow distribution characteristics of Z -type parallel channels were ...
Liang Yin, Jiaqiang E, Jie Ding
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Numerical Study on Regenerative Cooling Characteristics of Kerosene Scramjets [PDF]
The use of kerosene-based regenerative cooling for scramjet has been found widespread attention due to its inherent nature of high energy utilization efficiency and good thermal protection performance. In order to provide a reference for the later design and experiments, three-dimensional turbulence simulations and sensitivity analysis were performed ...
Xuan Jin, Chibing Shen, Xianyu Wu
doaj +3 more sources
Space storable regenerative cooling investigation [PDF]
Space storable regenerative cooling with FLOX/methane under conditions for small pump fed engine, describing injector and chamber ...
J. P. Mitchell, J. W. Neal
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Thermal-Structural Analysis of Regenerative Cooled Scramjet [PDF]
A numerical model is developed to quantitative evaluation of the thermal and structural characteristics of the regenerative cooled scramjet engine. The three-dimensional internal CFD platform for scramjet and the computational program of domestic aviation kerosene properties are incorporated together to develop three dimensional thermal evaluation code.
Ruoling Zhang, Jin Jiang, Feng Wang
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Cooling Performance Analysis of Regeneratively Cooled Combustion Chamber
A regenerative cooling system has been designed through empirical 1-D analysis for a liquid rocket engine of 30-ton-level thrust. The hot-gas-side wall temperature from 1-D analysis shows 100K difference compared to 3D CFD analysis. Two variations of design with same cooling performance are suggested for different maximum channel widths i.e., 4mm and ...
Woo-Seok Seol+2 more
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Design of Regenerative Cooled Cryogenic Rocket Engine [PDF]
The cryogenic rocket engine using propellants of liquid oxygen (LOX) and also the liquid hydrogen (LH2) category as produces the highest specific impulse has been designed, constructed which comprises of a pressure feed system, injector head assembly thrust chamber, and conical nozzle.
Aishwarya Dhara
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Mechanical oscillation and cooling actuated by the optical gradient force [PDF]
In this work we combine the large per-photon optical gradient force with the sensitive feedback of a high quality factor whispering-gallery microcavity.
Jessie Rosenberg+6 more
core +3 more sources
Working state map of hydrocarbon fuels for regenerative cooling
Regenerative cooling by endothermic hydrocarbon fuel (EHF) is one of the most promising techniques for thermal management of supersonic or hypersonic aircraft. How to maintain the fuel working in proper states is an important issue to maximize the cooling potential of EHT.
Chen Zhang+4 more
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Modeling and analysis of regenerative cooling channels for scramjet engine [PDF]
This paper presents a CFD simulation analysis method for the regenerative cooling channel of a supercombustion ramjet engine, and performs three-dimensional modeling and analysis. The influences of inlet mass flow, inlet pressure, and inlet temperature on the flow and heat transfer characteristics of kerosene in the cooling channel were analyzed, and ...
Xuefeng Xia+4 more
openaire +3 more sources