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Wind-tunnel investigation of an N.A.C.A. 23030 airfoil with various arrangements of slotted flaps / by I.G. Recant.

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Format:
Book
Government document
Author/Creator:
Recant, Isidore G., author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 755.
Technical note / National Advisory Committee for Aeronautics ; no. 755
Language:
English
Subjects (All):
Airplanes--Wings.
Airplanes.
Flaps (Airplanes).
Slotted flaps (Airplanes).
Wind tunnel testing.
Physical Description:
1 online resource (13 pages, 19 unnumbered pages) : illustrations.
Place of Publication:
Washington, [D.C.] : National Advisory Committee for Aeronautics, 1940.
Summary:
An investigation was made in the N.A.C.A. 7- by 10-foot wind tunnel of a large-chord N.A.C.A. 23030 airfoil with a 40- and a 25.66-percent-chord slotted flap to determine the section aerodynamic characteristics of the airfoil as affected by flap chord, slot shape, flap position, and flap deflections. The flap positions for maximum lift, the positions for minimum drag at moderate and high lift coefficients, and the complete section aerodynamic characteristics of selected optimum arrangements are given. Envelope polars of various flap arrangements are included. The relative merits of slotted flaps of different chords on the N.A.C.A. 23030 airfoil are discussed, and a comparison is made of each flap size with a corresponding flap size on the N.A.C.A. 23021 and 23012 airfoils.
Notes:
Description based on online resource, title from title screen (viewed May 29, 2020).
"March 1940."
"Langley Memorial Aeronautical Laboratory."
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: Recant, Isidore G. Wind-tunnel investigation of an N.A.C.A. 23030 airfoil with various arrangements of slotted flaps
OCLC:
1156324021

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