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Exact solutions in oscillating airfoil theoryA result obtained by Williams (1977) for two-dimensional airfoils oscillating in an arbitrary subsonic parallel flowfield is reformulated to show that the pressure distribution induced by any deformation can be construed from the particular solutions for heaving and pitching motions. Specific formulas are presented for an oscillating control surface with a sealed gap.
Document ID
19770053314
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Williams, M. H. (Princeton University Princeton, N.J., United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1977
Publication Information
Publication: AIAA Journal
Volume: 15
Subject Category
Aerodynamics
Accession Number
77A36166
Funding Number(s)
CONTRACT_GRANT: NGR-31-001-197
Distribution Limits
Public
Copyright
Other

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