Effects of Planform Geometry and Pivot Axis Location on the Aerodynamics of Pitching Low Aspect Ratio Wings
Author:
Affiliation:
1. University of Michigan, Ann Arbor
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2992
Reference23 articles.
1. Force coefficients for a NACA-0015 airfoil undergoing constant pitchrate motions
2. Graham, G.M. and Strickland, J.H. "An Experimental Investigation of an Airfoil Pitching at Moderate to HighRatestoLargeAnglesofAttack",24thAIAAAerospaceScienceMeeting,AIAA-86-0008.
3. Dynamic stall inception correlation for airfoils undergoing constantpitch rate motions
4. Unsteady flow past an airfoil pitching at a constant rate
5. Walker,J.M.andChou,D.C."ForcedUnsteadyVortexFlowsDrivenbyPitchingAirfoils",19thAIAAFluid Dynamics, Plasmaand Dynamicsand LasersConference,AIAA-87-1331.
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. Direct Force Measurements During Transient Flow about Pitching Flat Plates;55th AIAA Aerospace Sciences Meeting;2017-01-05
2. Parametric Variations in Aspect Ratio, Leading Edge and Planform Shapes for the Rectilinear Pitch Cases of AVT-202 (Invited);54th AIAA Aerospace Sciences Meeting;2016-01-02
3. Unsteady aerodynamic characteristics of a translating rigid wing at low Reynolds number;Physics of Fluids;2015-12
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