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Gas Film/Regenerative Composite Cooling Characteristics of the Lox/Lch4 Rocket Engine

https://doi.org/10.2139/ssrn.4113765
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21/21 checkable references clean · checked 2026-07-23

Every reference with a DOI in the deposited reference list resolved to a known work in Crossref or DataCite at the dated check, and none carried a retraction, withdrawal, or removal notice.

16 without a DOI — not checked. A reference deposited without a DOI is never matched by title or guessed at; it stays outside the checked set, and this line discloses that.

The 21 checked references that resolve
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Effect of artificial roughness on flow and heat transfer of transcritical methane
resolves10.1080/08916152.2014.945052
Experimental Investigation of Transient Forced Convection of Liquid Methane in a Channel at High Heat Flux Conditions
resolves10.1016/j.ijheatmasstransfer.2017.02.006
Transient responses of turbulent heat transfer of cryogenic methane at supercritical pressures
resolves10.1016/j.actaastro.2019.07.011
An experimental and modelling study of heat loads on a subscale methane rocket motor
resolves10.2514/1.T5865
Heat Transfer Prediction for Methane in Regenerative Cooling Channels with Neural Networks
resolves10.1016/j.actaastro.2020.05.008
Wall heat transfer prediction in CH4/O2 and H2/O2 rocket thrust chambers using a non-adiabatic flamelet model
resolves10.1016/j.csite.2021.101300
Numerical simulation for melting heat transport in nanofluids due to quadratic stretching plate with nonlinear thermal radiation
resolves10.1016/j.actaastro.2021.06.015
System scheme design of electric expander cycle for LOX/LCH4 variable thrust liquid rocket engine
resolves10.1080/10407780701364379
Numerical Study of Film and Regenerative Cooling in a Thrust Chamber at High Pressure
resolves10.1016/j.applthermaleng.2013.02.021
Numerical simulation of liquid film and regenerative cooling in a liquid rocket
resolves10.2514/3.23771
Effect of film cooling/regenerative cooling on scramjet engine performances
resolves10.2514/1.B35563
Thermal Behavior Inside Scramjet Cooling Channels at Different Channel Aspect Ratios
resolves10.1016/j.csite.2021.101664
Study on the heat transfer characteristics of regenerative cooling for LOX/LCH4 variable thrust rocket engine
resolves10.2514/1.T4299
Effect of Cooling Channel Aspect Ratio on Rocket Thermal Behavior
resolves10.1007/s11630-021-1369-8
A Correction Factor-Based General Thermal Resistance Formula for Heat Exchanger Design and Performance Analysis
resolves10.1016/j.ijthermalsci.2011.07.007
Experimental investigations of flow boiling heat transfer and pressure drop in straight and expanding microchannels – A comparative study
resolves10.1016/j.csite.2018.10.002
Study of heat transfer with surface treatment in pre-coolers for aeroengine applications
resolves10.1016/j.ijheatmasstransfer.2008.01.026
Refrigerant flow boiling heat transfer in parallel microchannels as a function of local vapor quality
resolves10.1080/01457630903312049
Mechanisms of Boiling in Micro-Channels: Critical Assessment
resolves10.1631/jzus.A1900468
Experimental investigation of nitrogen flow boiling heat transfer in a single mini-channel
resolves10.1016/0017-9310(79)90056-5
Film cooling from a single hole and a row of holes of variable pitch to diameter ratio
The 16 references without a DOI — listed, not checked
no DOI — not checkedref7
no DOI — not checkedEffect of inlet and outlet manifolds on regenerative cooling in LOX/Methane thrust chambers
no DOI — not checkedOn melting heat transport and nanofluid in a nozzle of liquid rocket engine with entropy generation
no DOI — not checkedCattaneo-Christov heat flux and entropy generation on hybrid nanofluid flow in a nozzle of rocket engine with melting heat transfer
no DOI — not checkedStudy on optimal gas film parameters of near-injection region in thrust chamber
no DOI — not checkedNumerical simulation of composite cooling of RBCC ejector rocket using gradient micro-channels
no DOI — not checkedref15
no DOI — not checkedNumerical simulation of liquid film and regenerative cooling in a rocket combustor
no DOI — not checkedChina material engineering grand ceremony
no DOI — not checkedModern engineering for design of liquid-propellant rocket engines
no DOI — not checkedInfluence of inlet water temperature on heat transfer and pressure drop of dehumidifying air coil using analytical and experimental methods
no DOI — not checkedTwo-phase frictional pressure drop with pure refrigerants in vertical mini/micro-channels
no DOI — not checkedref33
no DOI — not checkedref35
no DOI — not checkedLarge-eddy simulation of supersonic film cooling
no DOI — not checkedEffects of Combination of Forward Jet and Backward Jet with Two Rows of Holes on Film Cooling
What this badge says. CiteStamped means the CHECKABLE references of this work were clean at the dated check: each resolved to a known work in a public registry, and none carried a retraction notice at that time. It says nothing about the quality, findings, or importance of the work itself, and nothing about references deposited without a DOI.

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