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Blade Motion and Bouncing Tests of KD-1 AutogiroThere are forwarded herewith the results of blade motion and bouncing tests on the Kellett KD-1 three-bladed autogiro. Motion picture records and two-component accelerometer records were taken in flight during glides at air speeds from 30 miles per hour to 100 miles per hour indicator readings. Calibration curves of correct indicated air speed and rotor speed as functions of air speed meter reading were established with a trailing pitot-static head and a rotoscope, at 2,000 ft. altitude and an air density of 0.00231 slug/ cu. ft., all tests being made at approximately that density.
Document ID
20180002406
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Wheatley, John B.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
April 11, 2018
Publication Date
June 13, 1945
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-MR-X-1935
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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