Performance of Several Combustion Chambers Designed for Aircraft Oil Engines (1928)
NASA Technical Reports Server (NTRS) · leaf 12
to-cylinder orifice flared as noted above for speeds from 600 to 1,800 R. P. M. and for a constant fuel quantit}7 of 2.5 X 10"4 pounds per cycle, which is approximately 83 per cent of the full-load fuel charge. The I. M. E. P. throughout the entire range of speeds is approximately 110 pounds per… … Fuel quantify, lb./cycle Fig. 12.—Effect of load on engine performance. Fuel-injection perform- -Comparison of sharp and rounded orifice edges. Engine, Fig. 11. ance, cylinder head No. 3. Engine S. C.-L. T. E.; orifice, -rV-inch; LTE. Cylinder head No. 3; engine parts, standard; compression ratio,…
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