On helicopter in forward flight, inboard blade elements that pass through reverse flow region experience change in angle of attack of 360° once each revolution; in other flight conditions, angles of attack of fairly large areas of blades are beyond usual values for which data are customarily presented; program carried out to make available data for representative airfoil in unfamiliar range, at Reynolds Number close to flight conditions.
Forces and moments over NACA 0015 airfoil through 180° angle of attack
Aero Digest
Aero Digest ; 58 , n 4
1949
Article (Journal)
English
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