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The effect of lift, drag, and spinning characteristics of sharp leading edges on airplane wings / by Fred E. Weick and Nathan F. Scudder.

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Format:
Book
Government document
Author/Creator:
Weick, Fred E., author.
Scudder, Nathan F., author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 447.
Technical note / National Advisory Committee for Aeronautics ; No. 447
Language:
English
Subjects (All):
Airplanes--Wings.
Airplanes.
Leading edges (Aerodynamics).
Lift (Aerodynamics).
Drag (Aerodynamics).
Spin (Aerodynamics).
Physical Description:
1 online resource (15 pages, 9 unnumbered pages) : illustrations.
Place of Publication:
Washington, [D.C.] : National Advisory Committee for Aeronautics, 1933.
Summary:
In the spin tests in flight, which were made on a small training biplane, the addition of sharp leading edges produced favorable effects, causing a decrease in the angle of attack and rate of rotation and making the controls more effective. The flight and wind-tunnel tests agreed in showing that the use of the sharp leading edges is accomplished by a substantial reduction in the maximum lift coefficient.
Notes:
Description based on online resource, PDF version; title from title page (TRAIL, viewed January 11, 2021).
"February, 1933."
"Langley Memorial Aeronautical Laboratory."
"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).
Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
Other Format:
Print version: Weick, Fred E. The Effect of lift, drag, and spinning characteristics of sharp leading edges on airplane wings
OCLC:
1143006540

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