Reference health
Trade-off analysis of high-aspect-ratio-cooling-channels for rocket engines
18/18 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.
8 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 18 checked references that resolve
resolves10.2514/6.1993-1829
Numerical analysis of high aspect ratio cooling passage flow and heat transfer
resolves10.1016/S0065-2717(08)70153-9
Heat Transfer and Friction in Turbulent Pipe Flow with Variable Physical Properties
resolves10.2514/1.J052062
Effectiveness of Spalart–Allmaras Turbulence Model in Analysis of Curved Cooling Channels
resolves10.1080/10407782.2011.578011
A Quasi-2-D Model for the Prediction of the Wall Temperature of Rocket Engine Cooling Channels
resolves10.2514/1.B34533
Coupled Wall Heat Conduction and Coolant Flow Analysis for Liquid Rocket Engines
resolves10.2514/1.38542
Numerical Analysis of Three-Dimensional Flow of Supercritical Fluid in Cooling Channels
resolves10.1080/10407780903583016
Numerical Analysis of Deterioration in Heat Transfer to Near-Critical Rocket Propellants
resolves10.2514/6.2003-4613
Test Specimen Design and Measurement Technique for Investigation of Heat Transfer Processes in Cooling Channels of Rocket Engines Under Real Thermal Conditions
resolves10.2514/6.1997-2913
Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber
resolves10.2514/6.2001-3404
Thermo-and fluid mechanical analysis of high aspect ratio cooling channels
resolves10.2514/6.2003-4615
Experimental and Numerical Investigation of Thermal Stratification Effects
The 8 references without a DOI — listed, not checked
no DOI — not checkedHeat transfer in automobile radiators of the tubular type
no DOI — not checkedEsposito, J.J., Zabora, R.F., 1975. Thrust Chamber Life Prediction. Mechanical and Physical Properties of High Performance Rocket Nozzle Materials, vol. 1. NASA CR-134806. Final Report Boeing Aerospace Co., Seattle, WA.
no DOI — not checkedHarry III, D.P. 1963. Formulation and Digital Coding of Approximate Hydrogen Properties for Application to Heat-Transfer and Fluid-Flow Computations. Technical Report NASA TN D-1664.
no DOI — not checked10.1016/j.ijheatfluidflow.2013.08.003_b0030
no DOI — not checkedThermal stratification potential in rocket engine coolant channels
no DOI — not checkedOschwald, M., Suslov, D., Woschnak, A., 2005. Temperature Dependence of Material Properties and its Influence on the Thermal Distribution in Regeneratively Cooled Combustion Chamber Walls. 1st European Conference for Aerospace Sciences.
no DOI — not checkedComparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design
no DOI — not checkedThermophysical properties of fluids. I. Argon, ethylene, parahydrogen, nitrogen, nitrogen trifluoride, and oxygen
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work were clean at the dated check: each resolved to a known work in a public registry, and none
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