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Performance of a high-speed compression-ignition engine using multiple orifice fuel injection nozzles

Author: J A Spanogle; H H Foster; Langley Aeronautical Laboratory.
Publisher: Washington : National Advisory Committee for Aeronautics, [1930]
Series: Technical notes (United States. National Advisory Committee for Aeronautics), no. 344.
Edition/Format:   Book : National government publication : EnglishView all editions and formats
Database:WorldCat
Summary:
This report presents the test results during an investigation to determine the relative performance of a single-cylinder, high-speed, compression-ignition engine when using fuel injection valve nozzles with different numbers, sizes, and directions of round orifices. A spring-loaded, automatic injection value was used, centrally located at the top of a vertical disk-type combustion chamber formed between horizontally  Read more...
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Details

Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: J A Spanogle; H H Foster; Langley Aeronautical Laboratory.
OCLC Number: 26109250
Notes: Cover title.
"June, 1930."
Prepared at Langley Memorial Aeronautical Laboratory.
Description: 18 leaves, [21] leaves of plates : illustrations ; 27 cm.
Series Title: Technical notes (United States. National Advisory Committee for Aeronautics), no. 344.
Responsibility: by J.A. Spanogle and H.H. Foster.

Abstract:

This report presents the test results during an investigation to determine the relative performance of a single-cylinder, high-speed, compression-ignition engine when using fuel injection valve nozzles with different numbers, sizes, and directions of round orifices. A spring-loaded, automatic injection value was used, centrally located at the top of a vertical disk-type combustion chamber formed between horizontally opposed inlet and exhaust valves of a 5-inch by 7-inch engine.

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