Performance of Pure Fuels in a Single J33 Combustor PDF Download
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Author: Arthur L. Smith
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
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Author: Arthur L. Smith
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
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Author: Jerrold D. Wear
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 710
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Author: Edward G. Stricker
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 28
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The combustion efficiency and the altitude operational limits of three liquid hydrocarbon fuels having high volumetric energy content (decalin, tetralin, and monomethylnaphthalene) were compared with an AN-F-58 fuel in a single tubular combustor from a J33 turbojet engine. The investigation covered a range of simulated engine conditions for altitudes from 20,000 to 60,000 feet; 42- to 107-percent normal rated engine speed; and a flight Mach number of 0.6. The independent effects of combustor-inlet-air temperature, pressure, and mass air flow on the combustion efficiency of the fuels were determined around a standard combustion-inlet condition.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 52
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Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 922
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 26
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