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Analytic prediction of dynamic stall characteristics.A new approach is presented for solving the problem of predicting dynamic stall characteristics. In this approach, the unsteady aerodynamic characteristics are related theoretically to static aerodynamic characteristics which are readily available for a great number of airfoil shapes. Using these static experimental data as an input, the developed analytical method predicts dynamic stall characteristics that are in good agreement with available experimental data. The analysis is also extended to include frequency and amplitude modulation effects.
Document ID
19720050394
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ericsson, L. E.
Reding, J. P.
(Lockheed Missiles and Space Co., Inc. Sunnyvale, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 72-682
Report Number: AIAA PAPER 72-682
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Fluid and Plasma Dynamics Conference
Location: Boston, MA
Start Date: June 26, 1972
End Date: June 28, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A34060
Funding Number(s)
CONTRACT_GRANT: NAS1-9987
Distribution Limits
Public
Copyright
Other

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