The effect of injection-valve opening pressure on spray-tip penetration / by A.M. Rothrock and E.T. Marsh.

Format:

Book

Government document

Author/Creator:

Rothrock, A. M. (Addison May), 1903-1971, author.

Marsh, E. T., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 384.

Technical note / National Advisory Committee for Aeronautics ; No. 384

Language:

English

Subjects (All):

Nozzles.

Injectors.

Aerosols.

aerosol.

Medical Subjects:

Aerosols.

Physical Description:

1 online resource (4 pages, 3 unnumbered pages) : illustrations.

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1931.

Summary:

The effect of various injection-valve opening pressures on the spray-tip penetration was determined for several injection pressures. A common-rail fuel injection system was used for a given injection system was used. For a given injection pressure a maximum rate of penetration was obtained with an injection valve opening pressure equal to the injection pressure. As the excess of the injection pressure over the injection-valve opening pressure was increased for a given injection pressure, the effect of the injection-valve opening pressure on the spray-tip penetration was increased.

Notes:

Title from title screen (viewed February 5, 2020).

"July, 1931."

"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: Rothrock, A. M. (Addison May), 1903- The effect of injection-valve opening pressure on spray-tip penetration

OCLC:

1139565301