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Effect of Exhaust Pressure on Knock-limited Performance of an Air-cooled Aircraft-engine Cylinder

Albert M. LordOrville H. HeinickeEdward G. Stricker

出版	National Advisory Committee for Aeronautics, 1948
URL	http://books.google.com.hk/books?id=ffhzU5CUTi4C&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

The knock-limited inlet-manifold pressure and the mixture temperature corresponding to constant knock-limited inlet-manifold pressure were less sensitive to change in exhaust-to-inlet-manifold pressure ratio at a fuel-air ratio of 0.080 than at 0.066.