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The flight of an autogiro at high speedThis report presents a method for computing the flight performance of an autogiro at high speed, the velocity component along the blades being accounted for by calculation of the profile drag and the equation for zero torque.
Document ID
19930094688
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bennett, J A J
Date Acquired
September 6, 2013
Publication Date
December 1, 1933
Report/Patent Number
NACA-TM-729
Report Number: NACA-TM-729
Accession Number
93R23608
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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