Effects of varying the relative vertical position of wing and fuselage /

Effects of varying the relative vertical position of wing and fuselage /

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Bibliographic Details
Author / Creator:Prandtl, Ludwig, 1875-1953, author.
Imprint:[Washington, D.C.] : National Advisory Committee for Aeronautics, 1921.
Description:1 online resource (4 pages, 6 unnumbered pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 75
Technical note (United States. National Advisory Committee for Aeronautics) ; 75.
Subject:
Airplanes -- Wings.
Airplanes -- Fuselage.
Aerodynamics.
Mechanical efficiency.
Aerodynamics.
Airplanes -- Fuselage.
Airplanes -- Wings.
Mechanical efficiency.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12092554
Hidden Bibliographic Details
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"December, 1921."
"Extract from the First Report of the Gőttingen Aerodynamic Laboratory, Chap. IV, Sec. 7, pp. 118-120"--Page 1.
"Translated by the National Advisory Committee for Aeronautics"--Page 2.
No Federal Depository Library Program (FDLP) item number.
Description based on online resource, PDF version; title from title page (TRAIL, viewed February 6, 2020).
Other form:Print version: Prandtl, Ludwig, Effects of varying the relative vertical position of wing and fuselage
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/75

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