Comparison of Turbojet-engine Altitude Performance Characteristics and Ignition Limits with MIL-F-5624A Fuel, Grades JP-3 and JP-4 PDF Download
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Author: Willis M. Braithwaite
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
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Book Description
Author: Willis M. Braithwaite
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36
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Book Description
Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 28
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
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Book Description
Author: Edmund R. Jonash
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
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Book Description
Author: Harold R. Kaufman
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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Book Description
Author: Edward G. Stricker
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ISBN:
Category : Aeronautics
Languages : en
Pages : 28
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Book Description
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: Ivan D. Smith
Publisher:
ISBN:
Category :
Languages : en
Pages : 63
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Book Description
Author: Henry C. Barnett
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 46
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Book Description
Since the release of the first NACA publication of fuel characteristics pertinent to the design of aircraft fuel systems, additional information has become available on MIL-F-7914(AER) grade JP-5 fuel and several of the current grades of fuel oils. In order to make this information available to fuel-system designers as quickly as possible, the present report has been prepared as a supplement to NACA RM E53A21 "Fuel Characteristics Pertinent to the Design of Aircraft Fuel Systems" by Henry C. Barnett and R. R. Hibbard, 1953.
