[1]
Gui Y., Combined thermal phenomena of hypersonic vehicle. Scientia Sinica Physica, Mechanica & Astronomica, 2019, 49(11): 139–153.
[2]
Yang X., Xiao G., Du Y., Liu L., Wei D., Gui Y., Heat transfer with interface effects in high-enthalpy and high-speed flow: Modelling review and recent progress. Applied Thermal Engineering, 2021, 195: 116721.
[3]
Candler G.V., Rate effects in hypersonic flows. Annual Review of Fluid Mechanics, 2019, 51(1): 379–402.
[4]
Shinn J., Moss J., Simmonds A., Viscous-shock-layer heating analysis for the shuttle windward-symmetry plane with surface finite catalytic recombination rates. AIAA/ASME 3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference, St. Louis, Missouri, 1982, AIAA-82-0842.
[5]
Gupta R.N., Moss J.N., Simmonds A.L., Shinn J.L., Zoby E.V., Space shuttle heating analysis with variation in angle of attack and catalycity. Journal of Spacecraft and Rockets, 1984, 21(2): 217–219.
[6]
Steward D.A., Leiser D.B., Catalytic surface effect on ceramic coatings for an aeroassisted orbital transfer vehicle. Proceedings of the 8th annual conference on composites and advanced ceramic materials, John Wiley & Sons, Ltd, 1984, pp. 491–505.
[7]
Zoby E., Simmonds A., Gupta R., Temperature-dependent reaction-rate expression for oxygen recombination at shuttle entry conditions. AIAA 22nd Aerospace Sciences Meeting, Reno, Nevada, 1984, AIAA-84-0224.
[8]
Kovalev V.L., Kolesnikov A.F., Experimental and theoretical simulation of heterogeneous catalysis in aerothermochemistry (a review). Fluid Dynamics, 2005, 40(5): 669–693.
[9]
Nasuti F., Barbato M., Bruno C., Material-dependent catalytic recombination modeling for hypersonic flows. AIAA 28th Thermophysics Conference, Orlando, FL, 1993, AIAA-93-2840.
[10]
Kovalev V.L., Kolesnikov A.F., Krupnov A.A., Yakushin M.I., Analysis of phenomenological models describing the catalytic properties of high-temperature reusable coatings. Fluid Dynamics, 1996, 31(6): 910–919.
[11]
Kurotaki T., Construction of catalytic model on sio2-based surface and application to real trajectory. 34th Thermophysics Conference, Denver, CO, 2000, AIAA-2000-2366.
[12]
Armenise I., Barbato M., Capitelli M., Gorse C., Surface recombination coefficients and boundary-layer hypersonic-flow calculations on different surfaces. Journal of Spacecraft and Rockets, 2004, 41(2): 310–313.
[13]
Marschall J., MacLean M., Finite-rate surface chemistry model, i: Formulation and reaction system examples. 42nd AIAA Thermophysics Conference, Honolulu, Hawaii, 2011, AIAA-2011-3783.
[14]
Seward W.A., Jumper E.J., Model for oxygen recombination on silicon-dioxide surfaces. Journal of Thermophysics and Heat Transfer, 1991, 5(3): 284–291.
[15]
Willey R.J., Comparison of kinetic models for atom recombination on high-temperature reusable surface insulation. Journal of Thermophysics & Heat Transfer, 1993, 7(1): 55–62.
[16]
Yang X., Gui Y., Tang W., Du Y., Wei D., Xiao G., Liu L., Surface chemical effects on hypersonic nonequilibrium aeroheating in dissociated carbon-oxygen mixture. Journal of Spacecraft & Rockets, 2018, 55(3): 687–697.
[17]
Cacciatore M., Rutigliano M., Billing G.D., Eley-rideal and langmuir-hinshelwood recombination coefficients for oxygen on silica surfaces. Journal of Thermophysics and Heat Transfer, 1999, 13(2): 195–203.
[18]
Deutschmann O., Riedel U., Warnatz J., Modeling of nitrogen and oxygen recombination on partial catalytic surfaces. Journal of Heat Transfer, 1995, 117(2): 495–501.
[19]
Barbato M., Reggiani S., Bruno C., Muylaert J., Model for heterogeneous catalysis on metal surfaces with applications to hypersonic flows. Journal of Thermophysics and Heat Transfer, 2000, 14(3): 412–420.
[20]
Armenise I., Barbato M., Capitelli M., Kustova E., State-to-state catalytic models, kinetics, and transport in hypersonic boundary layers. Journal of Thermophysics and Heat Transfer, 2006, 20(3): 465–476.
[21]
Norman P., Schwartzentruber T., A computational chemistry methodology for developing an oxygen-silica finite rate catalytic model for hypersonic flows: Part ii. 43rd AIAA Thermophysics Conference, New Orleans, Louisiana, 2012, AIAA-2012-3097.
[22]
Li K., Liu J., Liu W., A new surface catalytic model for silica-based thermal protection material for hypersonic vehicles. Chinese Journal of Aeronautics, 2015, 28(5): 1355–1361.
[23]
Afonina N.E., Gromov V.G., Kovalev V.L., Investigation of the influence of different heterogeneous recombination mechanisms on the heat fluxes to a catalytic surface in dissociated carbon dioxide. Fluid Dynamics, 2002, 37(1): 117–125.
[24]
Guerra V., Analytical model of heterogeneous atomic recombination on silicalike surfaces. IEEE Transactions on Plasma Science, 2007, 35(5): 1397–1412.
[25]
MacLean M., Marineau E., Parker R., Dufrene A., Holden M., Desjardin P., Effect of surface catalysis on measured heat transfer in an expansion tunnel facility. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, Tennessee, 2012, AIAA-2012-0651.
[26]
Meng S., Zeng Q., Jin H., Wang L., Xu C., Evaluation of atomic oxygen catalytic coefficient of ZrB2-SiC by laser-induced fluorescence up to 1473 K. Measurement Science and Technology, 2018, 29(7): 075207.
[27]
Balat M.H., Czerniak M., Badie J.M., Ceramics catalysis evaluation at high temperature using thermal and chemical approaches. Journal of Spacecraft & Rockets, 1999, 36(2): 273–279.
[28]
Kim I., Park G., Experimental study of oxygen catalytic recombination on a smooth surface in a shock tube. Applied Thermal Engineering, 2019, 156: 678–691.
[29]
Stamatakis, Michail, Kinetic modelling of heterogeneous catalytic systems. Journal of Physics Condensed Matter, 2015, 27(1): 013001.
[30]
Keil F.J., Complexities in modeling of heterogeneous catalytic reactions. Computers & Mathematics with Applications, 2013, 65(10): 1674–1697.
[31]
Li Q., Phenomenological modeling of heterogeneous catalysis and numerical simulation of aerodynamic heating on aircraft surface. Shanghai Jiao Tong University, Shanghai, 2021.
[32]
Gui Y., Liu L., Dai G., Zhang L., Research status of hypersonic vehicle fluid-thermal-solid coupling and software development. Acta Aeronautica et Astronautica Sinica, 2017, 38(7): 020844.
[33]
Yang X., Guo Y., Tang W., Gui Y., Du Y., High-temperature real-gas effects and aerodynamic heating for capsules entering martian atmosphere. Journal of Astronautics, 2018, 39(9): 959–967.
[34]
Yang X., Gui Y., Qiu B., Du Y., Xiao G., Numerical investigation on influence of surface two-step catalytic mechanism on non-equilibrium aerodynamic heating for high-enthalpy CO2 flow. Journal of National University of Defense Technology, 2020, 42(1): 108–116.
[35]
Yang X., Hypersonic aerodynamic heating characterictics and coupling thermal effects for mars entry vehicles. China Aerodynamics Research and Development Center, Mianyang, 2017.
[36]
Turkel E., Van Leer B., Flux vector splitting and runge-kutta methods for the Euler equations. Ninth international conference on numerical methods in fluid dynamics. Springer Berlin Heidelberg, Berlin, Heidelberg, 1985, pp. 566–570.
[37]
Anderson W.K., Thomas J.L., Leer B.V., Comparison of finite volume flux vector splittings for the Euler equations. AIAA Journal, 1986, 24(9): 1453–1460.
[38]
Yoon S., Jameson A., An lu-ssor scheme for the euler and navier-stokes equations. 25th AIAA Aerospace Sciences Meeting, 1987, AIAA-87-0600.
[39]
Gupta R., Lee K., An aerothermal study of mesur pathfinder aeroshell. 6th Joint Thermophysics and Heat Transfer Conference, CoIorado Springs, CO, 1994, AIAA-94-2025.
[40]
Li Q., Yang X., Dong W., Du Y., Numerical simulation on influence of adsorption on surface heterogenerous catalysis process of hypersonic vehicle. Journal of Shanghai Jiao Tong University, 2021, 55(11): 1352–1361.
