Airfoil Flow Visualization and Pressure Measurements in High-Reynolds-Number Transonic Flow
Author:
Affiliation:
1. RWTH Aachen University, 52056 Aachen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2098
Reference15 articles.
Cited by 21 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
1. A Preliminary Study on Transonic Shock Tube Airfoil Flows with Gurney Flap by utilizing PDI;AIAA Scitech 2020 Forum;2020-01-05
2. Visualization study on vortex structure over an airfoil using planar laser induced fluorescence;Spectroscopy Letters;2018-08-09
3. Fundamental Study on Operational Parameters of Diaphragmless Shock Tube;MATEC Web of Conferences;2018
4. High-Speed Imaging of Shock Waves and Their Flow Fields;The Micro-World Observed by Ultra High-Speed Cameras;2017-09-01
5. Experimental Investigation of Shock Waves Formation and Development Process in Transonic Flow;Scientia Iranica;2017-08-29
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