Performance tests of a single-cylinder compression-ignition engine with a displacer piston (1935)
NASA Technical Reports Server (NTRS) · leaf 15
I.A.O.X. Technic*! Sot* lo. 518 Figs. 2,4,0 BOO 600 400 8 300 100 80- Oxaak angle, degrees Figure 3.- Relationship of air-flow speed to orank position and passage area during the compression stroke of a 5 by 7 engine with a 13-inch connecting rod. (Engine speed, 1,500 r.p.n.; dieplaoer height, 1… … Passage width, inch Figure 5.- Comparison of engine per- Figure 4.- Effect of passage width and injactlon-ralve formance with and without location on olear-exhaust engine performance. air flow. (8ingle-passage displacer,1,500 r.p.a.;. (Single-passage displacer,1,500 r.p.m.).
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
