Pressure distribution over a Clark Y-H airfoil section with a split flap / by Carl J. Wenzinger.

Format:

Book

Government document

Author/Creator:

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

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 627.

Technical note / National Advisory Committee for Aeronautics ; No. 627

Language:

English

Subjects (All):

Aerofoils.

Split flaps (Airplanes).

Aerodynamic load.

Wind tunnel testing.

Physical Description:

1 online resource (5 pages, 6 unnumbered pages) : illustrations.

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1937.

Summary:

An investigation was made in the N.A.C.A. 7- by 10-foot wind tunnel of the distributions of air pressure over one chord section of the Clark Y-H airfoil with a split flap. The results obtained are given in the form of diagrams showing the chordwise distribution of pressure on both airfoil and flap and as plots of calculated aerodynamic coefficients for both airfoil and flap.

Notes:

Description based on online resource, PDF version; title from title screen (viewed June 18, 2020).

"December 1937."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 5).

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. Pressure distribution over a Clark Y-H airfoil section with a split flap

OCLC:

1159597638