NASA NTRS · 19930090893
Experiments with a Wing Model from which the Boundary Is Removed by Suction
Abstract
The present report deals with a series of tests made for the purpose of improving flow conditions about wings by applying the suction principle (increase of the lift coefficient and reduction of the drag about very thick wing sections). Though not conclusive, the report contains interesting results.
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Schrenk, Oskar. 1929-10-01. Experiments with a Wing Model from which the Boundary Is Removed by Suction. https://ntrs.nasa.gov/citations/19930090893
Cite the original work for its findings. Save a collection to share your selection of sources.