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Some Effects of Injection Advance Angle, Engine-Jacket Temperature, and Speed on Combustion in a Compression-Ignition EngineAn optical indicator and a high-speed motion-picture camera capable of operating at the rate of 2,000 frames per second were used to record simultaneously the pressure development and the flame formation in the combustion chamber of the N. A. C. A. combustion apparatus. Tests were made at engine speeds of 570 and 1,500 r.p.m. The engine-jacket temperature was varied from 100° to 300° F. And the injection advance angle from 13° after top center to 120° before top center.

The results show that the course of the combustion is largely controlled by the temperature and pressure of the air in the chamber from the time the fuel is injected until the time at which combustion starts and by the ignition lag. The conclusion is presented that in a compression-ignition engine with a quiescent combustion chamber the ignition lag should be the longest that can be used without excessive rates of pressure rise; any further shortening of the ignition lag decreased the effective combustion of the engine.
Document ID
19930091598
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Report
Authors
A M Rothrock
(Langley Memorial Aeronautical Laboratory Hampton, United States)
C D Waldron
(Langley Memorial Aeronautical Laboratory Hampton, United States)
Date Acquired
September 6, 2013
Publication Date
January 15, 1935
Publication Information
Publisher: National Advisory Committee for Aeronautics
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
NACA-TR-525
Accession Number
93R20888
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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