Pressure distribution on wing ribs of the VE-7 and TS airplanes in flight / 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) ; 267.

Technical notes / National Advisory Committee for Aeronautics ; No. 267

Language:

English

Subjects (All):

Airplanes--Wings.

Airplanes.

Aerodynamic load.

Physical Description:

1 online resource (4 pages, 12 unnumbered pages) : illustrations.

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1927.

Summary:

This paper is the first of a series of notes, each of which presents the complete results of pressure distribution tests on single-wing ribs of the VE-7 and TS airplanes for a particular condition of flight. The level flight results are presented in the form of curves and show the comparison between the pressure distribution over a representative thin wing, R.A.F.-15, and a moderately thick wing, U.S.A.-27, throughout the range of angle of attack.

Notes:

Description based on online resource, PDF version; title from title page (TRAIL, viewed June 2, 2020).

"October 1927."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 4).

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

OCLC:

1127388928