Transonic flow past a symmetrical airfoil at high angle of attack
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, Calif.
2. NASA, Ames Research Center, Moffett Field; Spectron Development Laboratories, Inc., Costa Mesa, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-1500
Reference26 articles.
1. Transonic flow about a two-dimensional airfoil inviscid and turbulent flow properties
2. Experimental investigation of subsonic turbulent separated boundary layers on an airfoil
3. Flying-Hot-wire Study of Flow Past an NACA 4412 Airfoil at Maximum Lift
4. Steady and Unsteady Transonic Flow
Cited by 3 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. Self-sustained shock oscillations on airfoils at transonic speeds;Progress in Aerospace Sciences;2001-02
2. Transonic, turbulent boundary-layer separation generated on an axisymmetric flow model;AIAA Journal;1986-03
3. A comprehensive comparison between experiment and prediction for a transonic turbulent separated flow;13th Fluid and PlasmaDynamics Conference;1980-07-14
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