Effect of protruding gasoline tanks upon the characteristics of an airfoil / by Eastman N. Jacobs.

Format:

Book

Government document

Author/Creator:

Jacobs, Eastman N. (Eastman Nixon), 1902-1987, author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 249.

Technical notes / National Advisory Committee for Aeronautics ; No. 249

Language:

English

Subjects (All):

Airplanes--Fuel tanks.

Airplanes.

Aerofoils.

Drag (Aerodynamics).

Aerodynamics.

aerodynamics.

Physical Description:

1 online resource (2 pages, 3 unnumbered pages) : illustrations.

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1926.

Summary:

Uncertainty as to the effect of a gasoline tank protruding from the center section of a wing has led to the testing of such an arrangement in the variable density wind tunnel.

Notes:

Description based on online resource, PDF version; title from title page (TRAIL, viewed May 27, 2020).

"October 1926."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

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

Other Format:

Print version: Jacobs, Eastman N. Effect of protruding gasoline tanks upon the characteristics of an airfoil

OCLC:

1127388918