NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of air-entry angle on performance of a 2-stroke-cycle compression-ignition engineAn investigation was made to determine the effect of variations in the horizontal and vertical air-entry angles on the performance characteristics of a single-cylinder 2-stroke-cycle compression-ignition test engine. Performance data were obtained over a wide range of engine speed, scavenging pressure, fuel quantity, and injection advance angle with the optimum guide vanes. Friction and blower-power curves are included for calculating the indicated and net performances. The optimum horizontal air-entry angle was found to be 60 degrees from the radial and the optimum vertical angle to be zero, under which conditions a maximum power output of 77 gross brake horsepower for a specific fuel consumption of 0.52 pound per brake horsepower-hour was obtained at 1,800 r.p.m. and 16-1/2 inches of Hg scavenging pressure. The corresponding specific output was 0.65 gross brake horsepower per cubic inch of piston displacement. Tests revealed that the optimum scavenging pressure increased linearly with engine speed. The brake mean effective pressure increased uniformly with air quantity per cycle for any given vane angle and was independent of engine speed and scavenging pressure.
Document ID
19930081402
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Earle, Sherod L
Dutee, Francis J
Date Acquired
September 6, 2013
Publication Date
August 1, 1937
Report/Patent Number
NACA-TN-610
Report Number: NACA-TN-610
Accession Number
93R10692
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available