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Some experiments on autorotation of an airfoilThese experiments show that the rate of auto rotation of a monoplane airfoil is reduced by sweepback, ceasing entirely when the sweepback is 30 degrees. In addition a very serious increase in rate and range of auto rotation with yaw is shown.
Document ID
19930081167
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ober, Shatswell (Massachusetts Institute of Technology)
Date Acquired
September 6, 2013
Publication Date
September 1, 1929
Report/Patent Number
NACA-TN-319
Report Number: NACA-TN-319
Accession Number
93R10457
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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