Effect of Diffusion Fields on the Laminar Boundary Layer
Author:
Affiliation:
1. Bell Aircraft Corporation,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.2953
Reference19 articles.
Cited by 12 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. Influence of distributed heavy-gas injection on stability and transition of supersonic boundary-layer flow;Physics of Fluids;2019-10-01
2. On stability of the supersonic boundary layer with a foreign gas injection;AIP Conference Proceedings;2016
3. Some Effects of Injection of Foreign Gases in a Decelerating Laminar Boundary Layer in Supersonic Flow;Journal of the Aerospace Sciences;1962-10
4. Heat transfer, temperature recovery and skin friction on a flat plate with hydrogen release into a laminar boundary layer;International Journal of Heat and Mass Transfer;1961-12
5. Mass Transfer Cooling in a Boundary Layer;Aeronautical Quarterly;1961-05
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