The effect of lift, drag, and spinning characteristics of sharp leading edges on airplane wings /

The effect of lift, drag, and spinning characteristics of sharp leading edges on airplane wings /

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Bibliographic Details
Author / Creator:Weick, Fred E., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1933.
Description:1 online resource (15 pages, 9 unnumbered pages) : illustrations.
Language:English
Series:Technical note / National Advisory Committee for Aeronautics ; No. 447
Technical note (United States. National Advisory Committee for Aeronautics) ; 447.
Subject:
Airplanes -- Wings.
Leading edges (Aerodynamics)
Lift (Aerodynamics)
Drag (Aerodynamics)
Spin (Aerodynamics)
Airplanes -- Wings.
Drag (Aerodynamics)
Leading edges (Aerodynamics)
Spin (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12695168
Hidden Bibliographic Details
Other authors / contributors:Scudder, Nathan F., author.
United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"February, 1933."
"Part I - Wind-tunnel tests showing effect on lift, drag, and autorotation, by Fred E. Weick"--Pages 3-6.
"Part II - Flight tests showing effect on the spin and performance of the XN2Y-1 airplane, by Nathan F. Scudder"--Pages 6-11.
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 12).
Description based on online resource, PDF version; title from title page (TRAIL, viewed January 11, 2021).
Other form:Print version: Weick, Fred E. Effect of lift, drag, and spinning characteristics of sharp leading edges on airplane wings
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/447

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