Pressure drop across finned cylinders enclosed in a jacket / by Vern G. Rollin and Herman H. Ellerbrock, Jr.

Format:

Book

Government document

Author/Creator:

Rollin, Vern G., author.

Ellerbrock, Herman H., Jr., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 621.

Technical note / National Advisory Committee for Aeronautics ; No. 621

Language:

English

Subjects (All):

Internal combustion engines--Cylinders--Design and construction.

Internal combustion engines.

Pressure.

pressure.

Medical Subjects:

Pressure.

Physical Description:

1 online resource (18 pages, 9 unnumbered pages) : illustrations.

Place of Publication:

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

Summary:

The pressure drop across finned cylinders enclosed in a jacket for a range of air speeds from approximately 13 to 230 miles per hour has been investigated. Tests were made to determine the effect on the pressure drop of changes in fin space, fin width, fin shape, jacket entrance and exit areas, skirt-approach radius, and the use of fillets and a separator plate at the rear of the cylinder.

Notes:

Title from title screen (viewed June 18, 2020).

"November 1937."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 18).

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

Other Format:

Print version: Rollin, Vern G. Pressure drop across finned cylinders enclosed in a jacket

OCLC:

1159597632