LH941 发表于 2025-3-21 16:46:14

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法律 发表于 2025-3-21 22:23:31

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散开 发表于 2025-3-22 02:06:54

High-Enthalpy Testing in Hypersonic Shock Tunnels,einsam, daß die an sie vom Verbraucher gestellten Anforderungen erheblich angestiegen sind und sich teils sogar völlig gewandelt haben, weil auch die technischen Vorgänge, bei denen sie eingesetzt werden, eine Änderung erfahren haben, sei es, daß die Maschinen und Aggregate schneller arbeiten und da

赦免 发表于 2025-3-22 05:21:24

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Morsel 发表于 2025-3-22 09:53:12

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languid 发表于 2025-3-22 12:54:29

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

字谜游戏 发表于 2025-3-22 20:08:15

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

西瓜 发表于 2025-3-22 23:22:04

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HUMP 发表于 2025-3-23 03:53:06

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

思乡病 发表于 2025-3-23 05:51:40

https://doi.org/10.1007/978-1-4612-0379-7airplane; flow; numerical method; space; technology
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查看完整版本: Titlebook: Advances in Hypersonics; Defining the Hyperso John J. Bertin,Jacques Periaux,Josef Ballmann Book 1992 Springer Science+Business Media New Y