Pressure distribution on wing ribs of the VE-7 and TS airplanes in flight. Part II, Pull-ups. / by R.V. Rhode.

Format:

Book

Government document

Author/Creator:

Rhode, Richard V., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 277.

Technical notes / National Advisory Committee for Aeronautics ; No. 277

Language:

English

Subjects (All):

Airplanes--Wings.

Airplanes.

Aerodynamic load.

Physical Description:

1 online resource (6 pages, 55 unnumbered pages) : illustrations.

Other Title:

Pull-ups

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1928.

Summary:

This paper is the second in a series of notes, each of which presents the complete results of pressure distribution tests on wing and tail ribs of the VE-7 and TS airplanes for a particular manuever of flight. The results for pull-ups are presented in the form of curves which show the variation of pressure distribution, total loads, normal acceleration and center of pressure with respect to time.

Notes:

Description based on online resource, PDF version; title from title page (TRAIL, viewed June 3, 2020).

"January 1928."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 6).

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

Other Format:

Print version: Rhode, R. V. Pressure distribution on wing ribs of the VE-7 and TS airplanes in flight. Part 2: Pull-ups.

OCLC:

1127388952