找回密码
 To register

QQ登录

只需一步,快速开始

扫一扫,访问微社区

Titlebook: Symposium Transsonicum II; Göttingen, September Klaus Oswatitsch (o. Professor und Vorstand),Dietr Conference proceedings 1976 Springer-Ver

[复制链接]
楼主: 粗野的整个
发表于 2025-3-30 10:36:20 | 显示全部楼层
On the Motion of Shock Waves on an Airfoil with Oscillating Flapimensional attached transonic flow. It is shown that three different types of shock wave motion can be distinguished. An analytical model is developed, with which a satisfactory explanation can be given of the observed types of shock wave motion.
发表于 2025-3-30 14:35:31 | 显示全部楼层
发表于 2025-3-30 18:56:23 | 显示全部楼层
V. Karman Vortices and their Frequency Determination in the Wakes of Profiles in the Sub- and Transoduring transonic cascade research program in the AVA Göttingen it was found, that the wake flow behind the blades of turbine cascades and isolated profiles consists of v. Karman vortex streets under certain flow conditions. These vortices were visualized and analysed using a Schlieren system. Method
发表于 2025-3-30 23:08:11 | 显示全部楼层
发表于 2025-3-31 00:53:50 | 显示全部楼层
发表于 2025-3-31 06:22:34 | 显示全部楼层
发表于 2025-3-31 10:34:19 | 显示全部楼层
Review of the Application of Hodograph Theory to Transonic Aerofoil Design and Theoretical and Experare based, are summarized. The used mathematical methods lead to two different types of computation procedures; these are discussed..Typical computation results of a few advanced aerofoils are shown. As far as available, typical experimental results are also presented. An attempt is made to summariz
发表于 2025-3-31 16:30:50 | 显示全部楼层
Singular Perturbation Methods Applied to Two-Dimensional Transonic Flow around Slender Bodiesonviscous flow describing a transonic motion around slender bodies of finite length. The analytical solution determined by these methods is valid in the supersonic region of the flow field, in the near field as well as in the far field. Furthermore, at the surface of the body a first approximation o
发表于 2025-3-31 18:31:11 | 显示全部楼层
发表于 2025-4-1 01:20:54 | 显示全部楼层
Stabilization Law and Drag in Transonic Range of Velocitiesty of transonic flows, which they formulated as a stabilization law[.]. This law is confirmed by numerous wind tunnel tests, which were performed at different times in different countries. The most complete discussion of this experiments was given by Holder in 1964 in a lecture[.] commemorating the
 关于派博传思  派博传思旗下网站  友情链接
派博传思介绍 公司地理位置 论文服务流程 影响因子官网 SITEMAP 大讲堂 北京大学 Oxford Uni. Harvard Uni.
发展历史沿革 期刊点评 投稿经验总结 SCIENCEGARD IMPACTFACTOR 派博系数 清华大学 Yale Uni. Stanford Uni.
|Archiver|手机版|小黑屋| 派博传思国际 ( 京公网安备110108008328) GMT+8, 2025-5-7 02:19
Copyright © 2001-2015 派博传思   京公网安备110108008328 版权所有 All rights reserved
快速回复 返回顶部 返回列表