A comprehensive investigation of heat transfer in a high aspect ratio cooling channel of a rocket engine using LNG coolant
Tài liệu tham khảo
Neill, 2009, Practical uses of liquid methane in rocket engine applications, Acta Astronaut., 65, 696, 10.1016/j.actaastro.2009.01.052
Hong, 2019, An experimental and modelling study of heat loads on a subscale methane rocket motor, Acta Astronaut., 164, 112, 10.1016/j.actaastro.2019.07.011
Brown, 2004, Conceptual investigations for a methane -fueled expander rocket engine
Asakawa, 2017, The status of the research and development of LNG rocket engines in Japan, 463
Guzmán-Marmolejo, 2015, Methane in the solar system, Bol. Soc. Geol. Mex., 67, 377, 10.18268/BSGM2015v67n3a2
Shokri, 2018, Heat transfer aspects of regenerative-cooling in methane-based propulsion systems, Aero. Sci. Technol., 10.1016/j.ast.2018.09.025
Ruan, 2022, Numerical investigation on heat transfer and flow characteristics of supercritical methane in a horizontal tube, Cryogenics, 124, 10.1016/j.cryogenics.2022.103482
Xu, 2015, Numerical study of supercritical-pressure fluid flows and heat transfer of methane in ribbed cooling tubes, Int. J. Heat Mass Tran., 84, 346, 10.1016/j.ijheatmasstransfer.2015.01.041
Elmouazen, 2022, Heat transfer enhancement of hydrogen rocket engine chamber wall by using V-shape rib, Int. J. Hydrogen Energy, 47, 9775, 10.1016/j.ijhydene.2022.01.045
Elmouazen, 2022, Numerical investigation of pentagonal V-shape ribs to enhance heat transfer in hydrogen rocket engine cooling channels, Int. J. Hydrogen Energy, 47, 23871, 10.1016/j.ijhydene.2022.05.146
Urbano, 2014, Parametric analysis of cooling properties of candidate expander-cycle fuels, J. Propul. Power, 30, 153, 10.2514/1.B34852
Urbano, 2013, Numerical study of liquefied natural gas as a coolant in liquid rocket engines, Proc. Inst. Mech. Eng. G J. Aerosp. Eng., 227, 1130, 10.1177/0954410012451376
Li, 2022, Flow resistance characteristics of hydrocarbon fuel at supercritical pressure under various heat fluxes in regenerative cooling channel with micro-ribs, Aero. Sci. Technol., 131, 10.1016/j.ast.2022.107999
Santese, 2023, Impact of impurities on liquid methane properties under typical rocket operation conditions, International Journal of Thermofluids, 18, 10.1016/j.ijft.2023.100343
Pizzarelli, 2009, Numerical analysis of three-dimensional flow of supercritical fluid in cooling channels, AIAA J., 47, 2534, 10.2514/1.38542
Pizzarelli, 2010, Numerical analysis of deterioration in heat transfer to near-critical rocket propellants, Numer. Heat Tran., Part A: Applications, 57, 297, 10.1080/10407780903583016
Pizzarelli, 2013, Trade-off analysis of high-aspect-ratio-cooling-channels for rocket engines, Int. J. Heat Fluid Flow, 44, 458, 10.1016/j.ijheatfluidflow.2013.08.003
Pizzarelli, 2013, Coupled wall heat conduction and coolant flow analysis for liquid rocket engines, J. Propul. Power, 29, 34, 10.2514/1.B34533
Pizzarelli, 2015, Heat transfer modeling for supercritical methane flowing in rocket engine cooling channels, Appl. Therm. Eng., 75, 600, 10.1016/j.applthermaleng.2014.10.008
Votta, 2016, Experimental investigation of transcritical methane flow in rocket engine cooling channel, Appl. Therm. Eng., 101, 61, 10.1016/j.applthermaleng.2015.12.019
Leonardi, 2019, Analysis of thermal stratification impact on the design of cooling channels for liquid rocket engines, Int. J. Heat Mass Tran., 135, 811, 10.1016/j.ijheatmasstransfer.2019.02.028
Spalart, 1992, vol. 439
Younglove, 1987, Thermophysical properties of fluids. II. Methane, ethane, propane, isobutane, and normal butane, J. Phys. Chem. Ref. Data, 16, 577, 10.1063/1.555785
Pizzarelli, 2016, A CFD-derived correlation for methane heat transfer deterioration, Numer. Heat Tran., Part A: Applications, 69, 242, 10.1080/10407782.2015.1080575
Shokri, 2019, Improvement of heat-transfer correlations for supercritical methane coolant in rectangular channel, Appl. Therm. Eng., 147, 216, 10.1016/j.applthermaleng.2018.10.042
Silong Zhang, 2016, Thermal behavior inside scramjet cooling channels at different channel aspect ratios, J. Propul. Power, 32, 57, 10.2514/1.B35563
Zhang, 2016, Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios, Acta Astronaut., 127, 41, 10.1016/j.actaastro.2016.05.015
Li, 2020, Parametric analysis on the thermal behavior of cracking hydrocarbon fuel flow inside asymmetry heated cooling channels with micro-ribs, Int. J. Heat Mass Tran., 160, 10.1016/j.ijheatmasstransfer.2020.120154
Xu, 2018, Conjugate heat transfer, endothermic fuel pyrolysis and surface coking of aviation kerosene in ribbed tube at supercritical pressure, Int. J. Therm. Sci., 132, 209, 10.1016/j.ijthermalsci.2018.06.008
Ricci, 2016, Experimental and numerical investigation on the behaviour of methane in supercritical conditions, Appl. Therm. Eng., 107, 1334, 10.1016/j.applthermaleng.2016.07.052
Ricci, 2022, Transcritical behavior of methane in the cooling jacket of a liquid-oxygen/liquid-methane rocket-engine demonstrator, Energies, 15, 4190, 10.3390/en15124190
Gao, 2022, Thermal performance investigation of supercritical methane in minichannel heat sink on flight vehicle actuator under geometry effect of cross section, Numer. Heat Tran., Part A: Applications, 1
Gao, 2022, Heat transfer analysis of supercritical methane in microchannels with different geometric configurations on high power electromechanical actuator, J. Electron. Packag., 144, 10.1115/1.4053433
Haemisch, 2019, Experimental study of methane heat transfer deterioration in a subscale combustion chamber, J. Propul. Power, 10.2514/1.B37394
Haemisch, 2021, Experimental and numerical investigation of heat transfer processes in rocket engine cooling channels operated with cryogenic hydrogen and methane at supercritical conditions, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 19, 96, 10.2322/tastj.19.96
Heldens, 2021, On the characterization of methane in rocket nozzle cooling channels, Acta Astronaut., 186, 337, 10.1016/j.actaastro.2021.05.034
Votta, 2014, Experimental investigation of methane in transcritical conditions
Pizzarelli, 2023, Oxygen–methane rocket thrust chambers: review of heat transfer experimental studies, Acta Astronaut., 209, 48, 10.1016/j.actaastro.2023.04.028
Torres, 2008
Kuczyński, 2020, Impact of liquefied natural gas composition changes on methane number as a fuel quality requirement, Energies, 13, 5060, 10.3390/en13195060
Kunz, 2012, The GERG-2008 wide-range equation of state for natural gases and other mixtures: an expansion of GERG-2004, J. Chem. Eng. Data, 57, 3032, 10.1021/je300655b
Varzandeh, 2017, Comparison of GERG-2008 and simpler EoS models in calculation of phase equilibrium and physical properties of natural gas related systems, Fluid Phase Equil., 434, 21, 10.1016/j.fluid.2016.11.016
Huber, 2022, The NIST REFPROP database for highly accurate properties of industrially important fluids, Ind. Eng. Chem. Res., 61, 15449, 10.1021/acs.iecr.2c01427
Jiang, 2000, Critical temperatures and pressures for hydrocarbon mixtures from an equation of state with renormalization-group theory corrections, Fluid Phase Equil., 169, 127, 10.1016/S0378-3812(00)00299-5
Younglove, 1982, vol. 11
Lemmon, 2004, Viscosity and thermal conductivity equations for nitrogen, oxygen, argon, and air, Int. J. Thermophys., 25, 21, 10.1023/B:IJOT.0000022327.04529.f3
Olchowy, 1989, A simplified representation for the thermal conductivity of fluids in the critical region, Int. J. Thermophys., 10, 417, 10.1007/BF01133538
ANSYS FLUENT User's Guide," Release 13.0, ANSYS, Canonsburg, PA, Nov. 2010. 1985. http://www.ansys.com/.
Wilcox, 2008, Formulation of the k-w turbulence model revisited, AIAA J., 46, 2823, 10.2514/1.36541
Giovanetti, 1983
Oschwald, 2004