Technical Note
Published in The Aeronautical Journal • Jan 1, 1980
Authors:,
Ian Fejtek
John Nehera
Abstract
An experimental study was undertaken to measure the instantaneous lift and propulsive forces generated by a rigid, sinusoidally flapping wing at Reynolds numbers ranging from 72 000 to 120 000. The wing was flapped about a fulcrum at the root at frequencies of 2.55 Hz and 3.30 Hz. Instrumentation an...
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