NASA NTRS · 19780017149
Research on the statically thrusting propeller
Abstract
Methods for calculating the induced flow at propeller blades were analyzed by treating the wake formation as an initial problem in time. An unsteady vortex lattice technique was applied to the wake formation and the vortex core size was studied.
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Eisenhuth, J. J.. 1978-06-01. Research on the statically thrusting propeller. https://ntrs.nasa.gov/citations/19780017149
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