Stall Hysteresis of an Airfoil with Slotted Flap
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.11926
Reference14 articles.
1. Aerodynamic testing at low Reynolds numbers
2. An Overview of Static and Dynamic Airfoil Performance
3. Hysteresis effects on wind tunnel measurements of a two-element airfoil
4. Experimental Investigation of Multielement Airfoil Lift Hysteresis due to Flap Rigging
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2. Numerical and experimental analysis of the flow around a two-element wingsail at Reynolds number 0.53 × 106;International Journal of Heat and Fluid Flow;2016-12
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