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Titlebook: Numerical Simulation of Viscous Shock Layer Flows; Yuri P. Golovachov Book 1995 Springer Science+Business Media B.V. 1995 Navier-Stokes eq

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樓主
發(fā)表于 2025-3-21 17:04:16 | 只看該作者 |倒序瀏覽 |閱讀模式
書目名稱Numerical Simulation of Viscous Shock Layer Flows
編輯Yuri P. Golovachov
視頻videohttp://file.papertrans.cn/670/669197/669197.mp4
叢書名稱Fluid Mechanics and Its Applications
圖書封面Titlebook: Numerical Simulation of Viscous Shock Layer Flows;  Yuri P. Golovachov Book 1995 Springer Science+Business Media B.V. 1995 Navier-Stokes eq
描述The book is concerned with mathematical modelling of supersonic and hyper- sonic flows about bodies. Permanent interest in this topic is stimulated, first of all, by aviation and aerospace engineering. The designing of aircraft and space vehicles requires a more precise prediction of the aerodynamic and heat transfer characteristics. Together with broadening of the flight condition range, this makes it necessary to take into account a number of gas dynamic and physical effects caused by rarefaction, viscous-inviscid interaction, separation, various physical and chemical processes induced by gas heating in the intensive bow shock wave. The flow field around a body moving at supersonic speed can be divided into three parts, namely, shock layer, near wake including base flow, and far wake. The shock layer flow is bounded by the bow shock wave and the front and lat- eral parts of the body surface. A conventional approach to calculation of shock layer flows consists in a successive solution of the inviscid gas and boundary layer equations. When the afore-mentioned effects become important, implementation of these models meets difficulties or even becomes impossible. In this case, one ha
出版日期Book 1995
關(guān)鍵詞Navier-Stokes equation; dynamics; heat transfer; numerical methods; simulation
版次1
doihttps://doi.org/10.1007/978-94-015-8490-6
isbn_softcover978-90-481-4594-2
isbn_ebook978-94-015-8490-6Series ISSN 0926-5112 Series E-ISSN 2215-0056
issn_series 0926-5112
copyrightSpringer Science+Business Media B.V. 1995
The information of publication is updating

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沙發(fā)
發(fā)表于 2025-3-21 22:00:33 | 只看該作者
https://doi.org/10.1007/978-94-015-8490-6Navier-Stokes equation; dynamics; heat transfer; numerical methods; simulation
板凳
發(fā)表于 2025-3-22 03:57:45 | 只看該作者
978-90-481-4594-2Springer Science+Business Media B.V. 1995
地板
發(fā)表于 2025-3-22 05:47:29 | 只看該作者
Numerical Simulation of Viscous Shock Layer Flows978-94-015-8490-6Series ISSN 0926-5112 Series E-ISSN 2215-0056
5#
發(fā)表于 2025-3-22 12:07:53 | 只看該作者
Viscous shock layer models and computational methods,Such calculations can be carried out not only with the full Navier-Stokes equations but also with more simple mathematical models whose implementation requires a substantially smaller amount of computations.
6#
發(fā)表于 2025-3-22 16:27:45 | 只看該作者
Applications to plane and axisymmetric flows,er models. Most of them pertained to stationary flows about the bodies of revolution placed in a uniform supersonic stream. This chapter deals with simulation of more complicated viscous shock layer flows.
7#
發(fā)表于 2025-3-22 17:13:44 | 只看該作者
Simulation of three-dimensional flows,evere restrictions on the allowable value of time increment and the lower convergence rate of the iterative procedures as compared with one- and two-dimensional problems. For this reason, the well-founded use of gas dynamic models and numerical methods appears to be especially important.
8#
發(fā)表于 2025-3-23 00:16:38 | 只看該作者
Physical and chemical effects,ve physical and chemical processes which considerably influence the shock layer flow field and heat transfer. The examples of calculations are presented pertaining to spacecraft flight in the Earth and other planet atmospheres.
9#
發(fā)表于 2025-3-23 03:52:08 | 只看該作者
Book 1995irst of all, by aviation and aerospace engineering. The designing of aircraft and space vehicles requires a more precise prediction of the aerodynamic and heat transfer characteristics. Together with broadening of the flight condition range, this makes it necessary to take into account a number of g
10#
發(fā)表于 2025-3-23 08:41:48 | 只看該作者
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