Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil
Author:
Affiliation:
1. Department of Aerospace Engineering, Texas A&M University, College Station, Texas 77843-3141
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051673
Reference29 articles.
1. Progress in analysis and prediction of dynamic stall
2. Fluid mechanics of dynamic stall part I. Unsteady flow concepts
3. WatsonK.CormeyJ.KomerathN.DiOttavioJ. “Diagnostics of 3D Dynamic Stall on Rotor Blades,” Army Research Office TR-ARO-611102, 2008.
4. McAlisterK. W.CarrL. W.McCroskeyW. J. “Dynamic Stall Experiments on the NACA 0012 Airfoil,” NASA TP-1100, 1978.
5. Experimental and numerical investigations of dynamic stall on a pitching airfoil
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