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Energetics and optimum motion of oscillating lifting surfacesLow-frequency, unsteady, lifting-line theory is used to characterize the energetics and optimum motion of an unswept rigid wing oscillating harmonically in an inviscid, incompressible flow. The energetics calculations account for the leading edge suction force, the power absorbed in the wing oscillations, and the energy loss rate produced by vortex shedding. Optimization is achieved by minimizing the average energy loss rate in relation to a given thrust, and a unique solution is found in the three dimensional case for low, reduced frequencies. The two-dimensional solution is nonunique, a condition which is examined in terms of the normal modes of the energy loss rate matrix. An invisible mode with a hydrodynamic efficiency of 100 pct is obtained in the two-dimensional case, causing the nonuniqueness of the solution by yielding no fixed positive thrust through perfect unsteady feathering.
Document ID
19830055986
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ahmadi, A. R.
(Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Widnall, S. E.
(MIT Cambridge, MA, United States)
Date Acquired
August 11, 2013
Publication Date
July 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 83-1710
Accession Number
83A37204
Funding Number(s)
CONTRACT_GRANT: NGR-009-818
Distribution Limits
Public
Copyright
Other

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