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

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樓主: 選民
31#
發(fā)表于 2025-3-26 22:58:26 | 只看該作者
nged re-entry vehicles, air breathing hypersonic cruise and .This successful book gives an introduction to the basics of aerothermodynamics, as applied in particular to winged re-entry vehicles and airbreathing hypersonic cruise and acceleration vehicles. The book gives a review of the issues of tra
32#
發(fā)表于 2025-3-27 01:30:02 | 只看該作者
https://doi.org/10.1007/978-981-99-9191-4large. This does not mean that aerodynamic properties of hypersonic vehicles can be described fully by means of inviscid theory. This is at best possible for the longitudinal motion of re-entry vehicles.
33#
發(fā)表于 2025-3-27 06:33:04 | 只看該作者
https://doi.org/10.1007/978-981-99-9191-4-coupling exists to the state of the boundary layer. In particular the behavior of hydrodynamic stability, and hence laminar-turbulent transition, are affected by the thermal state of the surface, too.
34#
發(fā)表于 2025-3-27 13:07:01 | 只看該作者
https://doi.org/10.1007/978-981-99-9191-4 viscous flow and the inviscid flow. If, however, the boundary layerBoundary layer separates, the inviscid flowInviscid flow is changed and we observe a “strong interactionInteraction!strong|fc”. This phenomenon is present in all Mach number regimes, in particular also in the subsonic regime [1].
35#
發(fā)表于 2025-3-27 16:14:50 | 只看該作者
36#
發(fā)表于 2025-3-27 18:23:30 | 只看該作者
37#
發(fā)表于 2025-3-27 23:01:02 | 只看該作者
38#
發(fā)表于 2025-3-28 05:54:51 | 只看該作者
Multi-Span Long-Haul Transmissione “thermal state of the surface”, which—besides the classical similarity parameters—governs “thermal surface effects” on wall and near-wall viscousflow and thermo-chemical phenomena, as well as “thermal (heat) loads” on the structure.
39#
發(fā)表于 2025-3-28 08:41:45 | 只看該作者
Book 2015Latest edition hypersonic cruise and acceleration vehicles. The book gives a review of the issues of transport of momentum, energy and mass, real-gas effects as well as inviscid and viscous flow phenomena. In this second, revised edition the chapters with the classical topics of aerothermodynamics more or less we
40#
發(fā)表于 2025-3-28 11:40:25 | 只看該作者
Introduction,e “thermal state of the surface”, which—besides the classical similarity parameters—governs “thermal surface effects” on wall and near-wall viscousflow and thermo-chemical phenomena, as well as “thermal (heat) loads” on the structure.
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