The Effect of Engine Variables on the Preignition-limited Performance of Three Fuels PDF Download
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Author: Donald W. Male
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 7
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Book Description
Preignition-limited performance data for S reference fuel, diisobutylene, and benzene were obtained with an engine-heated hot spot on a supercharged CFR engine at 11 sets of engine operating conditions. Increases in compression ratio, spark advance, coolant temperature, or inlet-air temperature decreased the preignition-limited indicated mean effective pressure of all three fuels. Changes in the engine speed either raised or lowered the preignition-limited indicated mean effective pressure depending on the range of speed and the mixture strength. At nearly all the operating condiitons investigated, the order of the fuels according to increasing preignition-limited perfomrance was the same, that is, diisobutylene, benzene, and S reference fuel.
Author: Donald W. Male
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 7
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Book Description
Preignition-limited performance data for S reference fuel, diisobutylene, and benzene were obtained with an engine-heated hot spot on a supercharged CFR engine at 11 sets of engine operating conditions. Increases in compression ratio, spark advance, coolant temperature, or inlet-air temperature decreased the preignition-limited indicated mean effective pressure of all three fuels. Changes in the engine speed either raised or lowered the preignition-limited indicated mean effective pressure depending on the range of speed and the mixture strength. At nearly all the operating condiitons investigated, the order of the fuels according to increasing preignition-limited perfomrance was the same, that is, diisobutylene, benzene, and S reference fuel.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 916
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 490
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 210
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
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Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 206
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Author: Pai C. Hu
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 544
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(3) The Southwell plot method of predicting theoretical critical stresses for perfect specimens from experimental observations on actual specimens may not be expected to give, in general, satisfactory results when applied to flat plates.
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 664
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Author: Donald R. Bellman
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 210
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