Details of the Construction and Production of Fuel Pumps and Fuel Nozzles for the Airplane Diesel Engine (1936)
NASA Technical Reports Server (NTRS) · leaf 16
Figs. 10,11 N.A.C.A. Technical Memorandum No. 803 ,2pl03 Top position 3.14,10 Pitch of spiral 30 mm. Left handed spiral Pump discharge at 1800 r.p.m. Q = 16 kg /hr. qrp=340 mm ^(per injection) Figure 10.- Fuel pump valve developed.
NASA Technical Reports Server (NTRS)
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