Tests of N.A.C.A. airfoils in the variable density wind tunnel Series 44 and 64
Description:
This note is one of a series covering an investigation of a number of related airfoils. It presents the results obtained from tests in the N.A.C.A. Variable Density Wind Tunnel of two groups of six airfoils each. One group, the 44 series, has a maximum mean camber of 4 percent of the chord at a position 0.4 of the chord behind the leading edge and the other group, the 64 series, has a maximum mean camber of 6 percent of the chord at the same position. The members within each group differ only i…
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Date:
December 1931
Creator:
Jacobs, Eastman N. & Pinkerton, Robert M.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department