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U.S. Department of Energy
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Baseline performance and emissions data for a single-cylinder, direct-injected, diesel engine

Technical Report ·
OSTI ID:6497053
This report documents comprehensive fuel consumption, mean effective cylinder pressure, and emission test results for a supercharged, single-cylinder, direct-injected, four-stroke-cycle, diesel test engine. Inlet air-to-exhaust pressure ratios were varied from 1.25 to 3.35 in order to establish the potential effects of turbocharging techniques on engine performance. Inlet air temperatures and pressures were adjusted from 34/sup 0/ to 107/sup 0/C and from 193 to 414 kPa to determine the effects on engine performance and emissions. Engine output ranged from 300 to 2100 kPa (brake mean effective pressure) in the speed range of 1000 to 3000 rpm. Gaseous and particulate emission rates were measured. Real-time values of engine friction and pumping loop losses were measured independently and compared with motored engine values.
Research Organization:
National Aeronautics and Space Administration, Cleveland, OH (USA). Lewis Research Center
DOE Contract Number:
AI01-80CS50194
OSTI ID:
6497053
Report Number(s):
DOE/NASA/50194-38; NASA-TM-83638; ON: DE85001321
Country of Publication:
United States
Language:
English