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Vertical descent of the autogiroThe purpose of this report is to show that only part of the system of rotating blades really is in the "windmill decelerating attitude" when the profile drag is sufficiently low. This particular part receives more torque from the air loads than can be absorbed by the profile drag. As a result thereof the rotating autogiro blade, when its torque is zero, is in part a propeller which functions in the "annular vortex attitude."
Document ID
19930094743
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bennett, J A J
Date Acquired
September 6, 2013
Publication Date
June 1, 1932
Report/Patent Number
NACA-TM-673
Report Number: NACA-TM-673
Accession Number
93R23663
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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