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

選民

書目名稱Basics of Aerothermodynamics影響因子(影響力)




書目名稱Basics of Aerothermodynamics影響因子(影響力)學科排名




書目名稱Basics of Aerothermodynamics網(wǎng)絡公開度




書目名稱Basics of Aerothermodynamics網(wǎng)絡公開度學科排名




書目名稱Basics of Aerothermodynamics被引頻次




書目名稱Basics of Aerothermodynamics被引頻次學科排名




書目名稱Basics of Aerothermodynamics年度引用




書目名稱Basics of Aerothermodynamics年度引用學科排名




書目名稱Basics of Aerothermodynamics讀者反饋




書目名稱Basics of Aerothermodynamics讀者反饋學科排名

WITH

廣口瓶

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.

平庸的人或物

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”.

Frequency-Range

油氈

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.

Insubordinate

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

偏見

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”.

無禮回復

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

forebear

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