Titlebook: Basics of Aerothermodynamics; Ernst Heinrich Hirschel Book 2015Latest edition Springer International Publishing Switzerland 2015 Aerodynam

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Back-to-Back and Single-Span TransmissionExternal surfaces (the external flow path) of hypersonic flight vehicles primarily are radiation cooled. The radiation cooling effect depends on certain properties of the attached viscous flow, the boundary layer, and on the emissivity coefficient of the surface material.

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https://doi.org/10.1007/978-981-99-9191-4Fluid flow is characterized by transport of mass, momentum and energy. In this chapter we treat the transport of these three entities and its mathematical description in a basic way. Similarity parameters and, in particular, surface boundary conditions will be discussed in detail.

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Thermal Radiation Cooling of External Vehicle Surfaces,External surfaces (the external flow path) of hypersonic flight vehicles primarily are radiation cooled. The radiation cooling effect depends on certain properties of the attached viscous flow, the boundary layer, and on the emissivity coefficient of the surface material.

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Transport of Momentum, Energy, and Mass,Fluid flow is characterized by transport of mass, momentum and energy. In this chapter we treat the transport of these three entities and its mathematical description in a basic way. Similarity parameters and, in particular, surface boundary conditions will be discussed in detail.

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Viscous Thermal Surface Effects: Examples,The topic of thermal surface effects was introduced in Section 1.4. There the basic concept was explained and qualitative information was given. Quantitative information was presented in several of the following chapters. This chapter is devoted to a more in-depth consideration of several additional examples of viscous thermal surface effects.

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Ernst Heinrich HirschelSuccessful Introductory book in its second revised edition.Presents an introduction to the basics of aerothermodynamics, in particular to winged re-entry vehicles, air breathing hypersonic cruise and

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