The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals / by Max M. Munk.

Format:

Book

Government document

Author/Creator:

Munk, Max M. (Max Michael), 1890- author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 122.

Technical notes / National Advisory Committee for Aeronautics ; No. 122

Language:

English

Subjects (All):

Lift (Aerodynamics).

Angle of attack (Aerodynamics).

Aerofoils.

Camber (Aerofoils).

Physical Description:

1 online resource (9 pages, 2 unnumbered pages) : illustrations.

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1923.

Summary:

The integration is accomplished by the use of the mean camber of the section at particularly selected points. Simple graphical constructions of the zero directions are derived from the results.

Notes:

Title from title screen (viewed August 5 2019).

"January, 1923."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 1).

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

Other Format:

Print version: Munk, Max M. The Determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals

OCLC:

1111633657