Airplanes in horizontal curvilinear flight / by Heinrich Kann.

Format:

Book

Government document

Author/Creator:

Kann, Heinrich, author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 174.

Technical notes / National Advisory Committee for Aeronautics ; No. 174

Language:

English

Subjects (All):

Airplanes--Control surfaces.

Airplanes.

Airplanes--Flight testing.

Airplanes--Models--Aerodynamics.

Physical Description:

1 online resource (18 pages, 7 unnumbered pages) : illustrations

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1924.

Summary:

War airplanes require not only high speed and the ability to climb rapidly, but also the ability to traverse sharp curves quickly. An attempt is made, in the following note, to give a simple method of calculating horizontal curvilinear flight. A method for determining the area of the aileron and rudder surfaces will also be indicated. This discussion applies primarily to single and two-seater airplanes, although it can be extended to larger airplanes.

Notes:

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

"January, 1924."

"From Technische Berichte, Vol. III. No. 7."

"Translated by National Advisory Committee for Aeronautics"--Page 18

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references.

Print version record.

Other Format:

Print version: Kann, Heinrich. Airplanes in horizontal curvilinear flight /

OCLC:

1104148307