An Evaluation of Dynamic Stall Onset Prediction Methods for Rotorcraft Airfoil Design-Reference-Cited by-同舟云学术

An Evaluation of Dynamic Stall Onset Prediction Methods for Rotorcraft Airfoil Design

Published:2013-01-07 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Vieira Bernardo A.O.¹,Maughmer Mark D.¹

Affiliation:

1. The Pennsylvania State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1093

Reference14 articles.

1. [2]Leishman,J.G., PrinciplesofHelicopter Aerodynamics,2ndEdition,CambridgeUniversityPress,NY,2006.

2. [3]McCroskey, W. J.,McAlister,K.W., Carr,L. W.,Pucci,S.L.,Lambert, O.,andIndergrand, R.F."DynamicStallon Advanced Airfoil Sections,"Proceedings ofthe36th AnnualForumoftheAmericanHelicopterSociety, Washington DC, May1980.

3. [4]McCroskey, W. J.,McAlister,K.W., Carr,L. W.,and Pucci, S.L. "An ExperimentalStudyofDynamicStall onAdvanced Airfoil Sections," Volumes1,2&3NASA-TM-84245,1982.

4. [5]Martin,P.B.,Wilson,J.S.,Berry, J.D., Wong, T.C.,Moulton,M.,andMcVeigh,M.A."Passive Control ofCompressible DynamicStall,"AIAAPaper No.2008-7506, August,2008.

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