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Experiments with slotted wings.

U.S. Government Documents Available online

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Format:
Book
Government document
Author/Creator:
Lachmann, Gustav Victor, 1896- author.
Wieselsberger, Carl, author.
Katzmayr, Richard, 1884- author.
Kirste, Léon, author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 71.
Technical notes / National Advisory Committee for Aeronautics ; No. 71
Language:
English
Subjects (All):
Airplanes--Wings--Design and construction.
Airplanes.
Lift (Aerodynamics).
Physical Description:
1 online resource (32 pages, 4 unnumbered pages) : illustrations
Place of Publication:
[Washington, D.C]. : National Advisory Committee for Aeronautics, 1921.
Summary:
The idea of increasing the lift of an aerofoil by subdividing it goes back to gliding flight experiments by the writer before the war. A crash in August, 1917, with a Rumpler C airplane, on account of stalling, caused the idea to be put into concrete form and presented for a patent in 1918. The patent claim reads: "Supporting surface characterized by its being divided into a number of tandem components which together form a wing section." The application was at first rejected because the patent office did not believe in the possibility of increasing the lift by dividing the wing. The issuing patent was made dependent on conclusive proof of such increase.
Notes:
Title from title screen (viewed July 1, 2019).
"November, 1921."
"Translated from Zeitschrift fűr Flugtechnik und Motorluftschiffahrt, June 15, 1921 by the National Advisory Committee for Aeronautics."
"Slotted wing sections, by G. Lachmann of Darmstadt"--Page 1
"Gőttingen tests of Handley-Page wings, by C. Wieselsberger"--Page 17.
"Experiments with slotted wings, by R. Katzmayr and L. Kirste of Vienna"--Page 27
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical reference (page 7).
Print version record.
Other Format:
Print version: Lachmann, C. Experiments with slotted wings
OCLC:
1107323651

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