An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique
Author:
Affiliation:
1. NASA, Glenn Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-545
Reference9 articles.
Cited by 6 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. Effects of temperature on drag reduction in a subsonic turbulent boundary layer via micro-blowing array;Chinese Journal of Aeronautics;2022-09
2. Current state and prospects of researches on the control of turbulent boundary layer by air blowing;Progress in Aerospace Sciences;2015-07
3. Effect of micro-blowing of a gas from the surface of a flat plate on its drag;Journal of Applied Mechanics and Technical Physics;2012-07
4. Numerical Study on Flow Control by Micro-Blowing;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
5. Review of research into the concept of the microblowing technique for turbulent skin friction reduction;Progress in Aerospace Sciences;2004-11
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