Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plain ailerons and full-span split flaps / by Carl J. Wenzinger and Milton B. Ames, Jr.

Format:

Book

Government document

Author/Creator:

Wenzinger, Carl J. (Carl Joseph), 1903-1988, author.

Ames, Milton B., Jr., author.

Contributor:

United States. National Advisory Committee for Aeronautics, issuing body.

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 661.

Technical note / National Advisory Committee for Aeronautics ; No. 661

Language:

English

Subjects (All):

Airplanes--Wings--Testing.

Airplanes.

Split flaps (Airplanes).

Ailerons.

Wind tunnel testing.

Physical Description:

1 online resource (11 pages, 9 unnumbered pages) : illustrations.

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1938.

Summary:

An investigation was made in the N.A.C.A. 7- by 10-foott wind tunnel to determine the aerodynamic properties of rectangular and tapered N.A.C.A. 23012 wings with plain ailerons and a full-span split flap, the flap retracting ahead of the ailerons. Measurements were made of lift and drag and of pitching, rolling, yawing, and hinge moments for all conditions of full-span flaps neutral and deflected at different chord locations.

Notes:

Title from title screen (viewed June 18, 2020).

"August 1938."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 10).

Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.

Other Format:

Print version: Wenzinger, Carl J. Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plaine ailerons and full-span split flaps

OCLC:

1159597683