A THEORETICAL INVESTIGATION OF TURBULENT BOUNDARY LAYER FLOW WITH HEAT TRANSFER AT SUPERSONIC AND HYPERSONIC SPEEDS
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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. A theoretical and experimental investigation of the hypersonic turbulent boundary layer subject to normal and longitudinal pressure gradients and cross flow along a windward plane of symmetry;10th Aerospace Sciences Meeting;1972-01-17
2. Nonequilibrium regime of airflows in contoured nozzles - Theory and experiments;3rd and 4th Aerospace Sciences Meeting;1966-01-24
3. The Role of Unit Reynolds Number in Boundary-Layer Transition;Journal of the Aerospace Sciences;1959-03
4. Correlation of Base Pressure and Wake Structure of Sharp- and Blunt-Nose Cones with Reynolds Number Based on Boundary-Layer Momentum Thickness;Journal of the Aerospace Sciences;1959-03
5. The Viscous Flow Near a Stagnation Point When the External Flow Has Uniform Vorticity;Journal of the Aerospace Sciences;1959-02
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