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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
21#
發(fā)表于 2025-3-25 06:49:04 | 只看該作者
22#
發(fā)表于 2025-3-25 07:49:31 | 只看該作者
https://doi.org/10.1007/978-981-99-9191-4 into inviscid and viscous portions. At high altitudes this separation may become questionable. However, the central topic of this chapter is attached high speed viscous flow, whose basic properties are described with the help of the phenomenological model “boundary layer”.
23#
發(fā)表于 2025-3-25 12:16:24 | 只看該作者
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發(fā)表于 2025-3-25 16:00:32 | 只看該作者
Book 2015Latest editionrevised edition even more accentuates these topics. A new, additional chapter treats examples of viscous thermal surface effects. Partly only very recently obtained experimental and numerical results show the complexity of such phenomena (dependence of boundary-layer stability, skin friction, bounda
25#
發(fā)表于 2025-3-25 22:03:48 | 只看該作者
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發(fā)表于 2025-3-26 03:27:23 | 只看該作者
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發(fā)表于 2025-3-26 04:37:53 | 只看該作者
Inviscid Aerothermodynamic Phenomena,d and viscous portions. From Fig. 2.3, Section 2.1, we gather that the unit Reynolds numbers in the flight domain of interest are indeed sufficiently large. This does not mean that aerodynamic properties of hypersonic vehicles can be described fully by means of inviscid theory. This is at best possi
28#
發(fā)表于 2025-3-26 09:56:58 | 只看該作者
Attached High-Speed Viscous Flow, into inviscid and viscous portions. At high altitudes this separation may become questionable. However, the central topic of this chapter is attached high speed viscous flow, whose basic properties are described with the help of the phenomenological model “boundary layer”.
29#
發(fā)表于 2025-3-26 13:01:12 | 只看該作者
30#
發(fā)表于 2025-3-26 19:23:11 | 只看該作者
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