Abstract
The thermal state of the hypersonic vehicle surface governs on the one hand thermal surface effects (these are the influence of wall-temperature and temperature gradient in the gas at the wall on viscous and thermo-chemical phenomena at and near the vehicle surface) and on the other hand the thermal loads on the vehicle surface (regarding the structure and material layout of a TPS or a hot primary structure), Fig. 9.1 [1]. The thermal state of the surface indirectly governs also mechanical (pressure and shear stress) loads via its influence on primarily the wall-shear stress, for instance, in erosion processes at a TPS. This is, of course, a typical viscous thermal surface effect.
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References
Hirschel, E.H.: Basics of Aerothermodynamics. Progress in Astronautics and Aeronautics, AIAA, Reston, Va, vol. 204. Springer, Heidelberg (2004)
Goodrich, W.D., Derry, S.M., Bertin, J.J.: Shuttle Orbiter boundary layer Transition: A Comparison of Flight and Wind-Tunnel Data. AIAA-Paper 83-0485 (1983)
Wilcox, D.C.: Turbulence Modelling for CFD. DCW Industries, La Cañada, CAL, USA (1998)
Smits, A.J., Dussauge, J.-P.: Turbulent Shear Layers in Supersonic Flow, 2nd edn. AIP/Springer, New York (2004)
Neumann, R.D.: Defining the Aerothermodynamic Methodology. In: Bertin, J.J., Glowinski, R., Periaux, J. (eds.) Hypersonics. Defining the Hypersonic Environment, vol. 1, pp. 125–204. Birkhäuser, Boston (1989)
Hayes, J.R., Neumann, R.D.: Introduction to the Aerodynamic Heating Analysis of Supersonic Missiles. In: Mendenhall, M.R. (ed.) Tactical Missile Aerodynamics: Prediction Methodology. Progress in Astronautics and Aeronautics, AIAA, Reston, Va, pp. 63–110 (1992)
Bertin, J.J.: Hypersonic Aerothermodynamics. AIAA Education Series, Washington, D.C (1994)
Streit, T., Martin, S., Eggers, T.: Approximate Heat Transfer Methods for Hypersonic Flow in Comparison with Results Provided by Numerical Navier-Stokes Solutions. DLR FB 94-36 (1994)
Simeonides, G.: Generalized Reference-Enthalpy Formulation and Simulation of Viscous Effects in Hypersonic Flow. Shock Waves 8(3), 161–172 (1998)
Fujii, K.: Progress and Future Prospects of CFD in Aerospace – Wind Tunnel and Beyond. Progress in Aerospace Sciences 41(6), 455–470 (2005)
Haney, J.W.: Orbiter (Pre STS-1) Aeroheating Design Data Base Development Methodology: Comparison of Wind Tunnel and Flight Test Data. In: Throckmorton, D.A. (ed.) Orbiter Experiments (OEX) Aerothermodynamics Symposium. NASA CP-3248, Part 1, pp. 607–675 (1995)
Davy, W.C., Green, M.J.: A Review of the Infrared Imagery of Shuttle (IRIS) Experiment. In: Throckmorton, D. A. (ed.), Orbiter Experiments (OEX) Aerothermodynamics Symposium. NASA CP-3248, Part 1, pp. 215–232 (1995)
Throckmorton, D.A., Zoby, E.V.: Shuttle Infrared Leeside Temperature Sensing (SILTS) Experiment. In: Throckmorton, D. A. (ed.), Orbiter Experiments (OEX) Aerothermodynamics Symposium. NASA CP-3248, Part 1, pp. 233–248 (1995)
Throckmorton, D.A. (ed.): Orbiter Experiments (OEX) Aerothermodynamics Symposium. NASA CP-3248, Part 1 and 2 (1995)
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Hirschel, E.H., Weiland, C. (2009). The Thermal State of a Hypersonic Vehicle Surface. In: Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-89974-7_9
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