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Experimental transition investigation of a free-shear layer above a cavity at Mach 3.5

  • Published:1991-07 Issue:4 Volume:7 Page:626-634
  • ISSN:0748-4658
  • Container-title:Journal of Propulsion and Power
  • language:en
  • Short-container-title:Journal of Propulsion and Power

Author:

King Rudolph A.1,Creel Theodore R.1,Bushnell Dennis M.1

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23665

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,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. Stability of a hybrid mean velocity profile and its relevance to cavity resonance suppression;Physics of Fluids;2010-07

2. Cavity Tone Suppression Using a Rod in Cross Flow: investigation of Shear Layer Stability Mechanism;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

3. Development of Hypersonic Quiet Tunnels;Journal of Spacecraft and Rockets;2008-07

4. The Development of Hypersonic Quiet Tunnels;37th AIAA Fluid Dynamics Conference and Exhibit;2007-06-15

5. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies;Progress in Aerospace Sciences;2004-02
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