Effect of Engine Operating Conditions on the Vaporization of Safety Fuels (1932)
NASA Technical Reports Server (NTRS) · leaf 15
5Z{ Injection advance angle 5^ - 0^ B.T.C. "Engine tenrperature lOO'F 1-3 Q … 20 30 SO 60 10 Time - crankshaft degrees Fig.7 Effect of compression ratio on the vaporization of safety fuel. •>2
NASA Technical Reports Server (NTRS)
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