Flat plate boundary layer transition at hypersonic speeds
Author:
Affiliation:
1. DOUGLAS AIRCRAFT CO., INC., MISSILE AND SPACE SYSTEMS DIV., SANTA MONICA, CALIF.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1965-128
Cited by 26 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. Evaluation of nitric oxide laser-induced fluorescence thermometry techniques in a hypersonic boundary layer;Experiments in Fluids;2020-03-23
2. Hypersonic Transitional Shock-Wave–Boundary-Layer Interaction on a Flat Plate;AIAA Journal;2020-02
3. Numerical Simulations of a Cylinder-Induced Shock Wave/Boundary Layer Interaction;55th AIAA Aerospace Sciences Meeting;2017-01-05
4. A Conservation-Law Approach to Predicting the Length of the Boundary Layer Transition Region;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2012
5. Development of an Intermittency Equation for the Modeling of the Supersonic/Hypersonic Boundary Layer Flow Transition;Flow, Turbulence and Combustion;2011-03-01
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