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The comparative performance of an aviation engine at normal and high inlet air temperatures (1928)

NASA Technical Reports Server (NTRS) · leaf 5

An illustration from The comparative performance of an aviation engine at normal and high inlet air temperatures, 1928, leaf 5
412 REPOET NATIONAL ADVISOBY COMMITTEE FOE AERONAUTICS … 1400 WOO 1800 1400 1600 . 1800 1400 1600 laoo Revo/u-fions per minufe Revofuiions per minufe Revolufions per minufe Fig. 1—Liberty 12 engine. Full throttle power and fuel consunptioa at various air temperatures using a fuel mixture containing 30 per cent benzol and 70 per cent aviation gasoline.…

NASA Technical Reports Server (NTRS)

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