標(biāo)題: Titlebook: Advances in Hypersonics; Defining the Hyperso John J. Bertin,Jacques Periaux,Josef Ballmann Book 1992 Springer Science+Business Media New Y [打印本頁] 作者: LH941 時(shí)間: 2025-3-21 16:46
書目名稱Advances in Hypersonics影響因子(影響力)
書目名稱Advances in Hypersonics影響因子(影響力)學(xué)科排名
書目名稱Advances in Hypersonics網(wǎng)絡(luò)公開度
書目名稱Advances in Hypersonics網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Advances in Hypersonics被引頻次
書目名稱Advances in Hypersonics被引頻次學(xué)科排名
書目名稱Advances in Hypersonics年度引用
書目名稱Advances in Hypersonics年度引用學(xué)科排名
書目名稱Advances in Hypersonics讀者反饋
書目名稱Advances in Hypersonics讀者反饋學(xué)科排名
作者: 法律 時(shí)間: 2025-3-21 22:23 作者: 散開 時(shí)間: 2025-3-22 02:06
High-Enthalpy Testing in Hypersonic Shock Tunnels,einsam, da? die an sie vom Verbraucher gestellten Anforderungen erheblich angestiegen sind und sich teils sogar v?llig gewandelt haben, weil auch die technischen Vorg?nge, bei denen sie eingesetzt werden, eine ?nderung erfahren haben, sei es, da? die Maschinen und Aggregate schneller arbeiten und da作者: 赦免 時(shí)間: 2025-3-22 05:21 作者: Morsel 時(shí)間: 2025-3-22 09:53 作者: languid 時(shí)間: 2025-3-22 12:54
Christianities in the Trans-Atlantic Worldil with special consideration given to the Aachen tunnel. The basic shock tube performance is presented with numerical calculations using an equilibrium air model. The influence of boundary layer effects and van der Waals driver gas effects on the shock tube flow is included. Numerical calculations 作者: 字謎游戲 時(shí)間: 2025-3-22 20:08
Coda: Rachel Bernstein Goes to Surrey Laneh flight velocities impose severe problems on the flow field development and on the necessary simulation facilities. Vehicles, which strong influence of rarefaction effects on flight performance or on their design are作者: 西瓜 時(shí)間: 2025-3-22 23:22 作者: HUMP 時(shí)間: 2025-3-23 03:53
Coda: Rachel Bernstein Goes to Surrey Laned though little information is avilable for th transitional case. Reference is made to both experimental data and the growing volume of results from mathematical modelling..The main objective of the paper is to describe some of the difficult aerodynamic problems that the aircraft designer must on th作者: 思鄉(xiāng)病 時(shí)間: 2025-3-23 05:51
https://doi.org/10.1007/978-1-4612-0379-7airplane; flow; numerical method; space; technology作者: Extricate 時(shí)間: 2025-3-23 12:14
978-1-4612-6734-8Springer Science+Business Media New York 1992作者: Project 時(shí)間: 2025-3-23 16:40 作者: 可商量 時(shí)間: 2025-3-23 19:17
Breaking with Anthropocentrism: Genesis 1,In general, there are four primary reasons for wind tunnel testing:作者: innovation 時(shí)間: 2025-3-24 00:19
http://image.papertrans.cn/a/image/148305.jpg作者: Conclave 時(shí)間: 2025-3-24 03:31 作者: extrovert 時(shí)間: 2025-3-24 07:38
nics which took place in Colorado Springs and Aachen. The Second Course was organized at the US Air Force Academy, USA in January 1989 and the Third Course at Aachen, Germany in October 1990. The main idea of these Courses was to present to chemists, com- puter scientists, engineers, experimentalist作者: 牌帶來 時(shí)間: 2025-3-24 14:34
Coda: Rachel Bernstein Goes to Surrey Laneathematical modelling..The main objective of the paper is to describe some of the difficult aerodynamic problems that the aircraft designer must on the intake some of the somments are concerned with the nozzle and combustion chamber flows.作者: Decibel 時(shí)間: 2025-3-24 17:41 作者: 疲憊的老馬 時(shí)間: 2025-3-24 19:39
Book 1992 took place in Colorado Springs and Aachen. The Second Course was organized at the US Air Force Academy, USA in January 1989 and the Third Course at Aachen, Germany in October 1990. The main idea of these Courses was to present to chemists, com- puter scientists, engineers, experimentalists, mathema作者: 厚顏 時(shí)間: 2025-3-25 01:36
https://doi.org/10.1007/978-3-319-77194-6meter for hypersonic blunt bodies), and attitude on aerodynamic and aerothermodynamic characteristics are presented, and predictions from computational fluid dynamic (CFD) computer codes are compared with measurement.作者: BLUSH 時(shí)間: 2025-3-25 04:34
Christianities in the Trans-Atlantic Worldents and heat flux; time resolved flow visualization is possible. The experimental results given include nozzle calibrations and a study of the nozzle starting process. A table is included giving properties behind incident and reflected shocks at initial pressures of 0.01, 0.1 and 1 bar for equilibrium air.作者: figure 時(shí)間: 2025-3-25 09:18 作者: commodity 時(shí)間: 2025-3-25 13:01
Book 1992tems (including airbreathing systems), experimental methods for external and internal flow, theoretical and numerical methods. Since hyper- sonic flight requires highly integrated systems, the Short Courses not only aimed to give in-depth analysis of hypersonic research and technology but also tried作者: Affection 時(shí)間: 2025-3-25 19:46
ulsion systems (including airbreathing systems), experimental methods for external and internal flow, theoretical and numerical methods. Since hyper- sonic flight requires highly integrated systems, the Short Courses not only aimed to give in-depth analysis of hypersonic research and technology but also tried978-1-4612-6734-8978-1-4612-0379-7作者: Mindfulness 時(shí)間: 2025-3-25 21:38 作者: brother 時(shí)間: 2025-3-26 03:51 作者: 影響深遠(yuǎn) 時(shí)間: 2025-3-26 07:48 作者: 變量 時(shí)間: 2025-3-26 10:59 作者: 逗它小傻瓜 時(shí)間: 2025-3-26 13:48 作者: 大暴雨 時(shí)間: 2025-3-26 18:20
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