A numeric far field model for support interference studies in a slotted wall wind tunnel (European Transonic Windtunnel)
Author:
Affiliation:
1. Institute of Aerodynamics and Flow Technology, DLR Braunschweig, Lilienthalplatz 7, Braunschweig 38108, Germany.
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1243/09544100JAERO92
Reference1 articles.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
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3. Wind Tunnel Support System Influence on NASA Common Research Model at Low-Speed Conditions;Journal of Aircraft;2018-09
4. Wind Tunnel Support System Influence on NASA Common Research Model at Low Speed Conditions;32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2016-06-10
5. Computational tools for supporting the testing of civil aircraft configurations in wind tunnels;Progress in Aerospace Sciences;2008-02
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