Numerical Investigation of Deep Dynamic Stall for a Helicopter Blade Section
Author:
Affiliation:
1. New Mexico State University, Las Cruces, New Mexico 88003
Funder
Army Research Office
Army Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057686
Reference56 articles.
1. MODERN HELICOPTER AERODYNAMICS
2. Progress in analysis and prediction of dynamic stall
3. McCroskeyW. J. “The Phenomenon of Dynamic Stall,” NASA TM-81264, 1981.
4. CarrL. W.ChandrasekharaM. S.BrockN. J. “A Quantitative Study of Unsteady Compressible Flow on an Oscillating Airfoil,” AIAA Paper 1991-1683, 1991. doi:10.2514/6.1991-1683
5. Dynamic stall on a fully equipped helicopter model
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