Effect of Exhaust Pressure on the Performance of a 12-cylinder Liquid-cooled Engine PDF Download
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Author: Leland G. Desmon Publisher: ISBN: Category : Internal combustion engines Languages : en Pages : 530
Book Description
A dynamometer-stand investigation was conducted to determine the effect of exhaust pressure on the performance of a 12-cylinder liquid-cooled aircraft engine equipped with a conventional exhaust collector. The investigation covered a range of exhaust pressures from about 7 to approximately 62 inches of mercury absolute, engine speeds from 1600 to 3000 rpm, inlet-manifold pressures from 30 to 50 inches of mercury absolute and fuel-air ratios of 0.063, 0.069, 0.085, and 0.100.
Author: Leland G. Desmon Publisher: ISBN: Category : Internal combustion engines Languages : en Pages : 530
Book Description
A dynamometer-stand investigation was conducted to determine the effect of exhaust pressure on the performance of a 12-cylinder liquid-cooled aircraft engine equipped with a conventional exhaust collector. The investigation covered a range of exhaust pressures from about 7 to approximately 62 inches of mercury absolute, engine speeds from 1600 to 3000 rpm, inlet-manifold pressures from 30 to 50 inches of mercury absolute and fuel-air ratios of 0.063, 0.069, 0.085, and 0.100.
Author: Leland G. Desmon
Author: Leland G. Desmon
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: ![Society of Automotive Engineers [preprints]. PDF](https://books.google.com/books/content/images/frontcover/TovwJBUSMhUC?fife=w80-h100)
Author: 
Author: