Flow and Heat Transfer Characteristics of Hydrocarbon Fuel in Lightweight C/SiC Regenerative Cooling Combustor

[1]  J. Klemeš,et al.  Effect of pressure on regenerative cooling process of endothermic hydrocarbon fuel at severe pyrolysis conditions , 2023, Aerospace Science and Technology.

[2]  Yuguang Jiang,et al.  Influences of interconnection structure on the flow and heat transfer behaviors of the hydrocarbon fuel in parallel SCRamjet regenerative cooling channels , 2023, Numerical Heat Transfer, Part A: Applications.

[3]  J. Qin,et al.  Flow resistance characteristics of hydrocarbon fuel at supercritical pressure under various heat fluxes in regenerative cooling channel with micro-ribs , 2022, Aerospace Science and Technology.

[4]  Qiuwan Wang,et al.  Simplified pyrolytic model of RP-3 fuel at high conversion rates and the effects of primary reaction on the regenerative cooling process , 2022, Aerospace Science and Technology.

[5]  Kyu Hong Kim,et al.  Conjugate thermal analysis of X-51A-like aircraft with regenerative cooling channels , 2022, Aerospace Science and Technology.

[6]  Weixing Zhou,et al.  Characteristics of scramjet regenerative cooling with endothermic chemical reactions , 2022, Acta Astronautica.

[7]  Zhenguo Wang,et al.  Multidisciplinary design optimization of a wide speed range vehicle with waveride airframe and RBCC engine , 2021 .

[8]  G. Xie,et al.  Inhomogeneous behavior of supercritical hydrocarbon fuel flow in a regenerative cooling channel for a scramjet engine , 2021 .

[9]  Jian Liu,et al.  A review of regenerative cooling technologies for scramjets , 2021 .

[10]  H. Meng,et al.  Large eddy simulations and analyses of hydrocarbon fuel heat transfer in vertical upward flows at supercritical pressures , 2021 .

[11]  Q. Bi,et al.  Dynamic flow instabilities of hydrocarbon fuel in a horizontal heating tube , 2021 .

[12]  Sandra K. S. Boetcher,et al.  A review of heat transfer deterioration of supercritical carbon dioxide flowing in vertical tubes: Heat transfer behaviors, identification methods, critical heat fluxes, and heat transfer correlations , 2020 .

[13]  Tiantian Zhang,et al.  An analysis tool of the rocket-based combined cycle engine and its application in the two-stage-to-orbit mission , 2020 .

[14]  Yao Zheng,et al.  Asymmetric heating and buoyancy effects on heat transfer of hydrocarbon fuel in a horizontal square channel at supercritical pressures , 2019, Aerospace Science and Technology.

[15]  P. Jiang,et al.  Investigation of flow and heat transfer instabilities and oscillation inhibition of n-decane at supercritical pressure in vertical pipe , 2019, Applied Thermal Engineering.

[16]  O. Manca,et al.  On assessment of heat transfer deterioration of a channel with supercritical n-decane for scramjet engines cooling , 2019, International Journal of Heat and Mass Transfer.

[17]  Rui Li,et al.  Flow and thermal analyses of supercritical hydrocarbon fuel in curved regenerative cooling channel around cavity in rocket based combined cycle engine , 2018, Applied Thermal Engineering.

[18]  H. Meng,et al.  Conjugate heat transfer, endothermic fuel pyrolysis and surface coking of aviation kerosene in ribbed tube at supercritical pressure , 2018, International Journal of Thermal Sciences.

[19]  R. Xu,et al.  Review on active thermal protection and its heat transfer for airbreathing hypersonic vehicles , 2018, Chinese Journal of Aeronautics.

[20]  M. Pizzarelli.  The status of the research on the heat transfer deterioration in supercritical fluids: A review , 2018, International Communications in Heat and Mass Transfer.

[21]  F. Qin,et al.  Thermal analysis of regenerative-cooled pylon in multi-mode rocket based combined cycle engine , 2018, Acta Astronautica.

[22]  Jiang Qin,et al.  Performance evaluation of regenerative cooling/film cooling for hydrocarbon fueled scramjet engine , 2018, Acta Astronautica.

[23]  Weixing Zhou,et al.  Investigation on thermo-acoustic instability dynamic characteristics of hydrocarbon fuel flowing in scramjet cooling channel based on wavelet entropy method , 2018, Acta Astronautica.

[24]  Will O. Landsberg,et al.  Performance of high mach number scramjets - Tunnel vs flight , 2018 .

[25]  B. Ruan,et al.  Validation and analyses of RANS CFD models for turbulent heat transfer of hydrocarbon fuels at supercritical pressures , 2018 .

[26]  F. Qin,et al.  Flow and thermal analyses of regenerative cooling in non-uniform channels for combustion chamber , 2017 .

[27]  Jiang Qin,et al.  Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios , 2016 .

[28]  H. Meng,et al.  Numerical study of supercritical-pressure fluid flows and heat transfer of methane in ribbed cooling tubes , 2015 .

[29]  H. Meng,et al.  Analyses of surrogate models for calculating thermophysical properties of aviation kerosene RP-3 at supercritical pressures , 2015 .

[30]  Bala Vaidhyanathan,et al.  UHTC composites for hypersonic applications , 2014 .

[31]  Cheng-Hung Huang,et al.  The study on the improvement of system uniformity flow rate for U-type compact heat exchangers , 2013 .

[32]  Rong-pei Jiang,et al.  Thermal Cracking of Hydrocarbon Aviation Fuels in Regenerative Cooling Microchannels , 2013 .

[33]  Kai-Shing Yang,et al.  Characteristics of flow distribution in compact parallel flow heat exchangers, part I: Typical inlet header , 2011 .

[34]  Brian A. Maicke,et al.  Current State of High Speed Propulsion: Gaps, Obstacles, and Technological Challenges in Hypersonic Applications , 2009 .

[35]  Marc Bouchez,et al.  Ptah-socar fuel-cooled composite materials structure , 2008 .

[36]  D. Glass.  Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles , 2008 .

[37]  杨嘉陵,et al.  Research Progress On Thermal Protection Materials And Structures Of Hypersonic Vehicles , 2008 .

[38]  Edward Paquette.  Cooled CMC Structures for Scramjet Engine Flowpath Components , 2005 .

[39]  Marc Bouchez,et al.  PTAH-SOCAR Fuel-cooled Composite Materials Structure for Dual-Mode Ramjet and Liquid Rocket Engines - 2005 status , 2005 .

[40]  D. Van Wie,et al.  The hypersonic environment: Required operating conditions and design challenges , 2004 .

[41]  Shuuichi Ueda,et al.  Heating Evaluation Test of a Duct-shaped Cooling Structure Simulating Scramjet Combustors , 2004 .

[42]  C. Bouquet,et al.  Ceramic Matrix Composites Cooled Panel Development for Advanced Propulsion Systems , 2004 .

[43]  Clement Bouquet,et al.  Validation of a Leak-free C/SiC Heat Exchanger Technology , 2003 .

[44]  Marc Bouchez,et al.  PTAH-SOCAR Fuel-Cooled Composite Materials Structure in 2003 , 2003 .

[45]  A. Siebenhaar,et al.  The Strutjet engine - The overlooked option for space launch , 1995 .

[46]  Chi-Chuan Wang,et al.  Characteristics of fl ow distribution in compact parallel fl ow heat exchangers , part I : Typical inlet header , 2022 .