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Performance of Several Combustion Chambers Designed for Aircraft Oil Engines (1928)
NASA Technical Reports Server (NTRS) · leaf 8
7 PERFORMANCE OF COMBUSTION CHAMBERS Fig. 6.—Combustion chamber of Universal test engine … Pue/ guon/i/y, /b./cyc/e Fig. 5.—Effect of load on engine performance. Fuel-injection per- Fig. 7.—Fuel-injection performance, Universal test engine formance, cylinder head No. 2. Orifice, 1 inch; engine, S. C.-L. T.E.; compression ratio, 9.9; operating temperature, standard CYLINDER HEAD OF…NASA Technical Reports Server (NTRS)
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