Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps / by Hartley A. Soulé.

Format:

Book

Government document

Author/Creator:

Soule, Hartley A. (Hartley Akin), 1904-1988, author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 597.

Technical note / National Advisory Committee for Aeronautics ; No. 597

Language:

English

Subjects (All):

Airplanes--Tail surfaces--Mathematical models.

Airplanes.

Airplanes--Design and construction.

Flaps (Airplanes).

Airplanes--Tail surfaces.

Physical Description:

1 online resource (19 pages, 6 unnumbered pages) : illustrations.

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1937.

Summary:

A method of calculating the horizontal tail area for an airplane equipped with wing flaps is presented. The general problem of tail design, the effects of flaps on the factors involved, and the manner in which the flaps change the requirements upon which the minimum horizontal tail area is based are discussed.

Notes:

Description based on online resource, PDF version; title from title screen (viewed June 18, 2020).

"April 1937."

"Langley Memorial Aeronautical Laboratory."

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: Soule, Hartley A. (Hartley Akin), 1904-1988 Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps

OCLC:

1159597385