Variation of peak pitching-moment coefficients for six airfoils as affected by compressibility
Description:
Report presenting pressure distribution tests of six NACA 16-series propeller sections with 1-foot chords in the 8-foot high-speed tunnel to determine the compressibility effects on peak section pitching-moment coefficients. Data is presented as curves of peak section pitching-moment coefficient against Mach number, thickness ratio, and camber. The peak pitching-moment coefficients were found to occur in the regions of positive and negative stall.
Date:
October 1944
Creator:
Cleary, Harold E.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department