NASA NTRS · 19930094596
Some experiments on the slipstream effect
Abstract
The models designated "Torino 30, 31, 32" are horizontal tail surfaces of rectangular, triangular, and elliptical plan form and all of the same profile section. Tests were carried out with the object being to determine the effect of the propeller slipstream on the aerodynamical characteristics of the horizontal stabilizer. The results presented correspond to a first series of tests made without an interposed wing and in which the distance between the plane of the propeller disk and the tail was maintained constant.
Keep this discovery
Explore connections, maps & timelines
Ferrari, C. 1937-03-01. Some experiments on the slipstream effect. https://ntrs.nasa.gov/citations/19930094596
Cite the original work for its findings. Save a collection to share your selection of sources.