NASA NTRS ยท 19930090703
Testing a Windmill Airplane ("autogiro")
Abstract
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.
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Seiferth, R. 1927-01-01. Testing a Windmill Airplane ("autogiro"). https://ntrs.nasa.gov/citations/19930090703
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