Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section / by John A. Kelly and George B. McCullough.

Format:

Book

Government document

Author/Creator:

Kelly, John A., author.

McCullough, George B., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 3220.

Technical notes / National Advisory Committee for Aeronautics ; No. 3220

Language:

English

Subjects (All):

Aerodynamic load.

Aerofoils.

Flaps (Airplanes).

Leading edge flaps.

Leading edges (Aerodynamics).

Physical Description:

1 online resource (33 pages) : illustrations

Other Title:

Aerodynamic loads on a leading-edge flap and a leading-edge slat on the National Advisory Committee for Aeronautics 64A010 airfoil section

Place of Publication:

Washington [D.C.] : National Advisory Committee for Aeronautics, 1954.

Summary:

A previous report, NACA TN 3007, gave force and moment data for the NACA 64A010 airfoil section equipped alternately with a flap and a slat at the leading edge, and with a split flap and a double-slotted flap at the trailing edge. The present report presents the chordwise distributions of pressure measured concurrently with the force and moment data of NACA 3007. The pressure data for the leading-edge flap and slat have been converted into coefficients of normal force, chord force, and moment based on the geometry of the leading-edge device.

Notes:

Title from title screen (viewed June 7, 2019).

"June 1954."

"Ames Aeronautical Laboratory, Moffett Field, Calif."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 4).

Print version record.

Other Format:

Print version: Kelly, John A. Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section /

OCLC:

1104148259