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- W294611823 abstract "An investigation was conducted to compare the performance of two 25-ft-diam rotors which had identical dimensions and were similar in construction but different in blade airfoil-sections. Tests were conducted at indicated blade pitch angles from 3 degrees to 11.5 degrees and rotor speeds of 200, 290, and 371 rpm. The 23012.6 rotor required 2 percent less power to hover than the 0012.6. At thrust coefficients above design, the performance of the 23012.6 became better than the 0012.6 rotor." @default.
- W294611823 created "2016-06-24" @default.
- W294611823 creator A5071503543 @default.
- W294611823 date "1946-05-01" @default.
- W294611823 modified "2023-09-24" @default.
- W294611823 title "Static-thrust Investigation of Full-scale PV-2 Helicopter Rotors Having NACA 0012.6 and 23012.6 Airfoil Sections" @default.
- W294611823 hasPublicationYear "1946" @default.
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