Application of pulse facilities to inlet testing
Author:
Affiliation:
1. The Marquardt Corporation, Van Nuys, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.43589
Reference9 articles.
Cited by 11 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. UNSTEADY AND QUASI-STEADY MODES OF THE FLOW OVER AN INTAKE TESTED IN A HOTSHOT WIND TUNNEL;Journal of Applied Mechanics and Technical Physics;2023-10
2. Peculiarities of the flows forming in processes of an impulse starting of a supersonic wind tunnel with different diffusers;Thermophysics and Aeromechanics;2019-03
3. Sliding-Plug Approach for Inlet Self-Starting Ability Test in Shock Tunnel;AIAA Journal;2018-09
4. Starting processes at testing inlets in impulse wind tunnels;AIP Conference Proceedings;2018
5. A joint study on the starting limits of a generic supersonic inlet;47th AIAA Fluid Dynamics Conference;2017-06-02
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