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Titlebook: Advances in Hypersonics; Defining the Hyperso John J. Bertin,Jacques Periaux,Josef Ballmann Book 1992 Springer Science+Business Media New Y

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發(fā)表于 2025-3-21 16:46:14 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
期刊全稱Advances in Hypersonics
期刊簡(jiǎn)稱Defining the Hyperso
影響因子2023John J. Bertin,Jacques Periaux,Josef Ballmann
視頻videohttp://file.papertrans.cn/149/148305/148305.mp4
圖書封面Titlebook: Advances in Hypersonics; Defining the Hyperso John J. Bertin,Jacques Periaux,Josef Ballmann Book 1992 Springer Science+Business Media New Y
影響因子These three volumes entitled Advances in Hypersonics contain the Proceedings of the Second and Third Joint US/Europe Short Course in Hypersonics 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, experimentalists, mathematicians, and physicists state of the art lectures in scientific and technical dis- ciplines including mathematical modeling, computational methods, and experimental measurements necessary to define the aerothermo- dynamic environments for space vehicles such as the US Orbiter or the European Hermes flying at hypersonic speeds. The subjects can be grouped into the following areas: Phys- ical environments, configuration requirements, propulsion 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 tried
Pindex Book 1992
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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
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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
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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
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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
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https://doi.org/10.1007/978-1-4612-0379-7airplane; flow; numerical method; space; technology
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