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Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. X, Various control devices on a wing with a fixed auxiliary airfoil / by Fred E. Weick and Richard W. Noyes.

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Format:
Book
Government document
Author/Creator:
Weick, Fred E., author.
Noyes, Richard W., author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 451.
Technical note / National Advisory Committee for Aeronautics ; No. 451
Language:
English
Subjects (All):
Airplanes--Wings--Testing.
Airplanes.
Airplanes--Control surfaces.
Spoilers (Airplanes).
Wind tunnel testing.
Physical Description:
1 online resource (18 pages, 9 unnumbered pages) : illustrations.
Other Title:
Various control devices on a wing with a fixed auxiliary airfoil
Place of Publication:
Washington, [D.C.] : National Advisory Committee for Aeronautics, 1933.
Summary:
This is the tenth report on a series of systematic tests comparing lateral control devices with particular reference to their high angles of attack. The present tests were made with two sizes of ordinary ailerons and different sizes of spoilers on a Clark Y wing model having a narrow auxiliary airfoil fixed ahead and above the leading edge, the chords of the main and auxiliary airfoils being parallel. In addition, the auxiliary airfoil itself was given angular deflection for the purpose of providing rolling moments for lateral control.
Notes:
Description based on online resource, PDF version; title from title page (TRAIL, viewed January 11, 2021).
"March, 1933."
"Langley Memorial Aeronautical Laboratory."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (pages 15-16).
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. Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. X. Various control devices on a wing with a fixed auxiliary airfoil
OCLC:
1143006485

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