Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 / by M. J. Turner and S. Rabinowitz.

Format:

Book

Government document

Author/Creator:

Turner, M. J., author.

Rabinowitz, S., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 2213.

Technical notes / National Advisory Committee for Aeronautics ; No. 2213

Language:

English

Subjects (All):

Aerofoils.

Flaps (Airplanes).

Lift (Aerodynamics).

Pitching (Aerodynamics).

Hinge moments (Aerodynamics).

Physical Description:

1 online resource (46 pages) : illustrations.

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1950.

Summary:

Dietze's method for the solution of Possio's integral equation is used to determine the chordwise distribution of lift on an oscillating airfoil with simple hinged flap in two-dimensional compressible flow (subsonic). Results of these calculations are used to prepare tables of aerodynamic coefficients for lift, pitching moment (referred to quarter-chord point), and flap hinge moment for a Mach number of 0.7; the motions considerd are vertical translation, airfoil rotation about a quarter-chord point, and rotation of the flap about its hinge line.

Notes:

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

"October 1950"

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 19).

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

Other Format:

Print version: Turner, M. J., Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7

OCLC:

1100474485