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Analysis of flight and wind-tunnel tests on Udet airplanes with reference to spinning characteristicsThis report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were determined for the effectiveness of all the controls at various angles of attack. The autorotation was studied by subjecting the rotating model to an air blast.
Document ID
19930090821
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Herrmann, H
Date Acquired
September 6, 2013
Publication Date
March 1, 1929
Report/Patent Number
NACA-TM-502
Report Number: NACA-TM-502
Accession Number
93R20111
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLIGHT & WIND TUNNEL
SPINNING TESTS - UDET
AUTOROTATION TESTS - UDET WIND TUNNEL
AUTOROTATION & SPINNING
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