NASA NTRS · 19710050392
A method for predicting helicopter wake geometry, wake-induced flow and wake effects on blade airloads
Abstract
Wake model and computer program to compute geometries, flows and velocity influence coefficients for helicopter blade load calculations
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Sadler, S. G.. 1971-05-01. A method for predicting helicopter wake geometry, wake-induced flow and wake effects on blade airloads. https://ntrs.nasa.gov/citations/19710050392
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