Development of the Junkers-diesel Aircraft Engine (1930)
NASA Technical Reports Server (NTRS) · leaf 25
Figs. 15,17 & 20 N.A.C.A. Technical Memorandum No. 565 … f Inta>o Fig, 15 Section through fuel pump S 300 0E- 'Power curve 2 d CQ d CQ p 1555/A / /> 14707 •H +3 S? ^100° > o 0 1 I i -L CO 0.4 0.8 1.2 1.6 Vol. of air drawn in,m^/s Fig. 17 Characteristic curves of rotary s ovfire ngiiig pump F03. 0 [*1 Fig. 20 Inertia sysiesa of two shaft angine
NASA Technical Reports Server (NTRS)
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