A REVIEW OF THE ROLE OF SOME SMALL HIGH-SPEED WIND TUNNELS IN AERONAUTICAL RESEARCH
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,Aerospace Engineering
Cited by 10 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. Force measurement using strain-gauge balance in shock tunnel based on deep learning;Chinese Journal of Aeronautics;2023-08
2. Design of an experimental wind tunnel system for control applications;International Journal of Electrical Engineering & Education;2018-09-12
3. Force Measurements and Computational Validation of a Transonic Wing-Tip Flow;Journal of Aircraft;2016-11
4. Force Measurements on a NACA 0012 Wingtip at Mach 0.75;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
5. Surface Flow Visualization of a Side-Mounted NACA 0012 Airfoil in a Transonic Ludwieg Tube;28th International Symposium on Shock Waves;2012
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