Publications of Dr. Kevin D. Jones:
Presented at the 9th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines,
Ecole Centrale de Lyon, Lyon, France, September 4-8, 2000
Title: THE UNSTEADY AERODYNAMICS OF FLAPPING-FOIL PROPELLERS
Authors: M.F. Platzer and K.D. Jones
Abstract:
It is the objective of this paper to summarize the authors' recent work on flapping
foils. Water tunnel experiments on sinusoidally plunging foils are described which
elucidate the change in vortical wake pattern shed from the foil's trailing edge. These
experiments were carried out using dye flow visualization and laser-Doppler velocimetry.
It is found that the wake pattern is a strong function of the maximum non-dimensional plunge
velocity, with the wake topology changing from a typical Kármán vortex street to an
inverse Kármán vortex street to an asymmetric wake structure as the non-dimensional
plunge velocity increases. These results are partly reproducible with inviscid panel
code and Navier-Stokes code predictions. Additional interesting features are obtained if
two degrees of freedom are permitted (pitch-plunge motions). Depending
on the pitch/plunge amplitudes and the phasing between the two motions, the foil either
produces thrust or extracts energy. A water tunnel experiment is described which
demonstrates the possibility of power generation from a slowly flowing, shallow river.
Additional interesting features are found if two airfoils in close proximity to each
other are studied. Experiments with two airfoils arranged in a biplane configuration
and oscillating in counter-phase show significant thrust and propulsive benefits in comparison
to single flapping foils.
Download a complete copy of the paper in PostScript (compressed) (1.0MB) format
or PDF (1.1MB) format.

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