Development of the Junkers-diesel Aircraft Engine (1930)
NASA Technical Reports Server (NTRS) · leaf 22
t/ Figs, 4,9 & 10 N.A.C.A. Technical Memorandum No• 565 Ai reraft e nginc> Aut onob ile c ngi no 0 __P_0]70^ _ _ „ hp St rvt i our., ry engine Displacement 1 Piston speed,m/s Weight " hp" Fig. 4 Juniors double-piston engine … die p i ae 3 ae nt V>, o 30° 40c 60° Incidence of scavenging ports. Fig.9 Effect of varying rotation of scavenging air on the combustion.
NASA Technical Reports Server (NTRS)
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