Force tests on and airflow surveys near autogiro rotor in NACA full-scale wind tunnel; force tests made at three pitch settings and several rotor speeds; effect of fairing protuberances on rotor blade; induced downwash and yaw angles at two tip-speed ratios in plane 1 1/2 ft above path of blade tips. (Price 5¢)
Full-scale wind-tunnel tests of PCA-2 autogiro rotor
Nat Advisory Committee Aeronautics -- Report
1935
10 pages
Bibliography
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Full-scale wind-tunnel tests of a PCA-2 autogiro rotor
TIBKAT | 1935
|Wind-Tunnel Tests of 10-foot-diameter Autogiro Rotors
NTRS | 1937
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|Wind-tunnel tests of a 10-foot-diameter autogiro rotors
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