Effect of aerofoil aspect ratio on the slope of the lift curve / by Walter S. Diehl.

Format:

Book

Government document

Author/Creator:

Diehl, Walter S. (Walter Stuart), 1893-1976, author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 79.

Technical notes / National Advisory Committee for Aeronautics ; No. 79

Language:

English

Subjects (All):

Aerofoils.

Aerofoils--Mathematical models.

Aspect ratio (Aerofoils).

Lift (Aerodynamics).

Physical Description:

1 online resource (4 pages, 1 unnumbered page) : illustration.

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1922.

Summary:

One of the most important characteristics of an aerofoil is the rate of change of lift with angle of attack. This tactor determines the effectiveness of a tail plane in securing static longitudinal stability.

Notes:

Title from title screen (viewed July 1, 2019).

"January, 1922."

No Federal Depository Library Program (FDLP) item number.

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

Other Format:

Print version: Diehl, Walter S. Effect of aerofoil aspect ratio on the slope of the lift curve

OCLC:

1107323716