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An experimental study of dynamic stall on advanced airfoil section. Volume 2: Pressure and force dataExperimentally derived force and moment data are presented for eight airfoil sections that were tested at fixed and varying incidence in a subsonic two dimensional stream. Airfoil incidence was varied through sinusoidal oscillations in pitch over a wide range of amplitude and frequency. The surface pressure distribution, as well as the lift, drag, and pitching moment derived therefrom, are displayed in a uniform fashion to delineate the static and dynamic characteristics of each airfoil both in and out of stall.
Document ID
19830003778
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mcalister, K. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Pucci, S. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Mccroskey, W. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Carr, L. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
USAAVRADCOM-TR-82-A-8-VOL-2
NASA-TM-84245-VOL-2
NAS 1.15:84245-VOL-2
A-8925
Accession Number
83N12048
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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