Wind-Tunnel Tests of a 10-foot-diameter Gyroplane Rotor (1936)
NASA Technical Reports Server (NTRS) · leaf 9
6 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Tip-speed ratio, p Figure 8.- -Rotor angle of attack a as a function of tip-speed ratio, 10-foot gyro- plane rotor, four blades. 036 c: 032 028 Q O § .024 ./ .2 .3 .4 .5 .6 .7 .8 .9 o Tip-speed ratio, p k 020 Figure 11.—Lateral-force coefficient CV of 10-foot gyroplane rotor, four blades. o to 0/6…
NASA Technical Reports Server (NTRS)
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