Reference health
Numerical simulation and optimization on heat transfer and fluid flow in cooling channel of liquid rocket engine thrust chamber
17/17 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.
11 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 17 checked references that resolve
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Turbulent heat transfer in a serpentine channel with a series of right-angle turns
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Three-dimensional flow analysis in a rocket engine coolant channel of high depth/width ratio
resolves10.1016/S0094-5765(03)80021-8
Technology developments for thrust chambers of future launch vehicle liquid rocket engines
resolves10.2514/6.1994-3103
A concurrent multi-disciplinary approach for the analysis of liquid rocket engine combustors
resolves10.2514/6.1993-1829
Numerical analysis of high aspect ratio cooling passage flow and heat transfer
resolves10.1175/1520-0493(1963)091<0099:GCEWTP>2.3.CO;2
GENERAL CIRCULATION EXPERIMENTS WITH THE PRIMITIVE EQUATIONS
resolves10.1016/0029-5493(95)01153-6
Numerical prediction of augmented turbulent heat transfer in an annular fuel channel with repeated two-dimensional square ribs
resolves10.2514/6.1992-3151
Numerical analysis of the hot-gas-side and coolant-side heat transfer in liquid rocket engine combustors
resolves10.1299/jsmecmd.2003.16.177
303 Numerical Simulation on Heat Transfer and Fluid Flow in Cooling Channel of Liquid Rocket Engine Thrust Chamber
resolves10.1016/0017-9310(91)90020-F
Evaporative cooling of liquid film through interfacial heat and mass transfer in a vertical channel—I. Experimental study
resolves10.1016/S0009-2509(01)00050-1
Numerical simulation of the high Reynolds number slit nozzle gas–particle jet using subgrid-scale coupling large eddy simulation
resolves10.1016/j.ijheatmasstransfer.2005.06.017
Numerical study of liquid film cooling in a rocket combustion chamber
The 11 references without a DOI — listed, not checked
no DOI — not checkedBartz, D.R. (1957), “A simple equation for rapid estimation of rocket nozzle convective heat transfer coefficients”, Jet Propulsion, Vol. 27 No. 1, pp. 49‐51.
no DOI — not checkedFeng, W.L. and Zhang, Y.J. (1991), Theory of Liquid Rocket Engine, BeiHang University Press, BeiJing (in Chinese).
no DOI — not checkedKinney, G.R. and Dukler, A.E. (1952), “Internal liquid film cooling experiments with air stream temperatures to 2000F in 2‐ and 4‐inch diameter horizontal tubes”, NACA Report.
no DOI — not checkedKnuth, E.L. (1953), “The mechanics of film cooling”, JPL Memo, September, pp. 20‐85.
no DOI — not checkedLi, J.W. and Liu, Y. (2004), “Method of computing temperature field in regeneration‐cooled thrust chamber”, Journal of Aerospace Power, Vol. 19 No. 4, pp. 550‐6.
no DOI — not checkedLilly, D.K. (1966), “On the application of the eddy viscosity concept in the inertial subrange of turbulence”, NCAR Manuscript 123, National Center for Atmospheric Research, Boulder, CO.
no DOI — not checkedTao, W.Q. (2000), Numerical Heat Transfer, 2nd ed., Xi'an Jiaotong University Press, Xi'an (in Chinese).
no DOI — not checkedWang, T.S. and Luong, V. (2004), “Numerical a study on the cooling mechanism in liquid rocket engine”, paper presented at 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit; Fort Lauderdale, FL, July, pp. 11‐4.
no DOI — not checkedWilliam, M.G. (1991), “Liquid film cooling in rocket egines”, CD Report, March.
no DOI — not checkedWu, F., Wang, Q.W., Luo, L.Q. and Sun, J.G. (2005a), “Numerical investigation of turbulent models on heat transfer and fluid flow in cooling channel of H2/O2 liquid rocket engine thrust chamber”, Journal of Propulsion Technology, Vol. 26 No. 5, pp. 389‐93.
no DOI — not checkedWu, F., Wang, Q.W., Luo, L.Q. and Sun, J.G. (2005b), “Numerical simulation on heat transfer and fluid flow in cooling channel of liquid propellant rocket engine thrust chamber”, Journal of Aerospace Power, Vol. 20 No. 4, pp. 197‐202.
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