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Testing a Windmill Airplane ("autogiro")In order to clear up the matter ( In the Spanish report it was stated that the reference surface for the calculation of the coefficients c(sub a) and c(sub w) was the area of all four wings, instead of a single wing), the model of a windwill airplane was tested in the Gottingen wind tunnel.
Document ID
19930090703
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Seiferth, R
Date Acquired
September 6, 2013
Publication Date
January 1, 1927
Report/Patent Number
NACA-TM-394
Report Number: NACA-TM-394
Accession Number
93R19993
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES, WIND TUNNEL TESTS - AUTOGIROS, WIND TUNNEL TESTS
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