標(biāo)題: Titlebook: Basics of Aerothermodynamics; Ernst Heinrich Hirschel Book 2015Latest edition Springer International Publishing Switzerland 2015 Aerodynam [打印本頁(yè)] 作者: 選民 時(shí)間: 2025-3-21 19:18
書(shū)目名稱Basics of Aerothermodynamics影響因子(影響力)
書(shū)目名稱Basics of Aerothermodynamics影響因子(影響力)學(xué)科排名
書(shū)目名稱Basics of Aerothermodynamics網(wǎng)絡(luò)公開(kāi)度
書(shū)目名稱Basics of Aerothermodynamics網(wǎng)絡(luò)公開(kāi)度學(xué)科排名
書(shū)目名稱Basics of Aerothermodynamics被引頻次
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書(shū)目名稱Basics of Aerothermodynamics讀者反饋
書(shū)目名稱Basics of Aerothermodynamics讀者反饋學(xué)科排名
作者: WITH 時(shí)間: 2025-3-21 23:49 作者: 廣口瓶 時(shí)間: 2025-3-22 03:09
Real-Gas Aerothermodynamic Phenomena,ypersonic flight usually is defined as flight at Mach numbers . 5. Here appreciable real-gas effects begin to appear. In this chapter we discuss the important real-gas phenomena with the goal to understand them and their implications in vehicle design.作者: 平庸的人或物 時(shí)間: 2025-3-22 06:12
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”.作者: Frequency-Range 時(shí)間: 2025-3-22 10:52 作者: 油氈 時(shí)間: 2025-3-22 12:57
https://doi.org/10.1007/978-981-99-9191-4ypersonic flight usually is defined as flight at Mach numbers . 5. Here appreciable real-gas effects begin to appear. In this chapter we discuss the important real-gas phenomena with the goal to understand them and their implications in vehicle design.作者: Insubordinate 時(shí)間: 2025-3-22 20:40
https://doi.org/10.1007/978-981-99-9191-4d 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作者: 偏見(jiàn) 時(shí)間: 2025-3-23 00:10
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”.作者: 無(wú)禮回復(fù) 時(shí)間: 2025-3-23 02:13
https://doi.org/10.1007/978-981-99-9191-4 cooled. The thermal state governs thermal surface effects and thermal loads, as well as the skin friction. Regarding the thermal state, a strong back-coupling exists to the state of the boundary layer. In particular the behavior of hydrodynamic stability, and hence laminar-turbulent transition, are作者: forebear 時(shí)間: 2025-3-23 08:56
https://doi.org/10.1007/978-981-99-9191-4nces the pressure field, i.e., the inviscid flowInviscid flow field, only weakly. We call this “weak interactionInteraction!weak” between the attached viscous flow and the inviscid flow. If, however, the boundary layerBoundary layer separates, the inviscid flowInviscid flow is changed and we observe作者: Expiration 時(shí)間: 2025-3-23 11:08 作者: 難解 時(shí)間: 2025-3-23 17:14
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.作者: Debility 時(shí)間: 2025-3-23 21:58
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.作者: Control-Group 時(shí)間: 2025-3-24 00:55 作者: disrupt 時(shí)間: 2025-3-24 05:05 作者: 主講人 時(shí)間: 2025-3-24 08:55
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.作者: 休戰(zhàn) 時(shí)間: 2025-3-24 13:56
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.作者: 食物 時(shí)間: 2025-3-24 17:20
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.作者: 音樂(lè)學(xué)者 時(shí)間: 2025-3-24 20:48
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 作者: acrophobia 時(shí)間: 2025-3-25 01:56 作者: 參考書(shū)目 時(shí)間: 2025-3-25 06:49 作者: 蔓藤圖飾 時(shí)間: 2025-3-25 07:49
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”.作者: 親密 時(shí)間: 2025-3-25 12:16 作者: Autobiography 時(shí)間: 2025-3-25 16:00
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作者: FACET 時(shí)間: 2025-3-25 22:03 作者: 會(huì)犯錯(cuò)誤 時(shí)間: 2025-3-26 03:27 作者: etidronate 時(shí)間: 2025-3-26 04:37
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作者: 防銹 時(shí)間: 2025-3-26 09:56
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”.作者: FER 時(shí)間: 2025-3-26 13:01 作者: callous 時(shí)間: 2025-3-26 19:23 作者: CROW 時(shí)間: 2025-3-26 22:58
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作者: 法律 時(shí)間: 2025-3-27 01:30
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.作者: phase-2-enzyme 時(shí)間: 2025-3-27 06:33
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.作者: Saline 時(shí)間: 2025-3-27 13:07
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].作者: FECK 時(shí)間: 2025-3-27 16:14 作者: Freeze 時(shí)間: 2025-3-27 18:23 作者: 航海太平洋 時(shí)間: 2025-3-27 23:01 作者: Amylase 時(shí)間: 2025-3-28 05:54
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.作者: Inordinate 時(shí)間: 2025-3-28 08:41
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作者: 整體 時(shí)間: 2025-3-28 11:40
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.作者: 里程碑 時(shí)間: 2025-3-28 18:10
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