Engine performance with a hydrogenated safety fuel (1933)
NASA Technical Reports Server (NTRS) · leaf 11
Fuel quantity, lb./cycle Figure 3.- b.m.e.p. and fuel consumption obtained at compression ratios of 5.0, 5.5 and 6.0 with a valve overlap of 112" using aviation gasoline at atmospheric intake pressure and using safety fuel at atmospheric intake pressure and 2 inches of mercury boost pressure.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
