Turbulent Separated Flow Over a Rounded Divergent Trailing Edge

Author:

Hunter Andrew1,Thompson Brian2

Affiliation:

1. Rensselaer Polytechnic Institute

2. ThermalCentric

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. Influence of Boundary-Layer Thickness on Base Pressure and Vortex Shedding Frequency

2. Whitcomb, R.T. "Review of NASA Supercritical Airfoils," ICAS 74-10, August1974.

3. Supercritical Wing Sections II

4. Harris, C.D. "Wind tunnel Investigation of Effects of Trailing Edge Geometry on a NASA Supercritical Airfoil Section," NASA. TM-X2336,Jan.1971.

5. Henne, P.A., and Gregg, R.D. "New Airfoil Design Concept," Journal of Aircraft, May1991,pp.300-311.

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