Author: Richard J. McCafferty
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Liquid-fuel-distribution and Fuel-state Effects on Combustion Performance of a Single Tubular Combustor
Author: Richard J. McCafferty
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Vapor-fuel-distribution Effects on Combustion Performance of a Single Tubular Combustor
Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Combustion Efficiency and Altitude Operational Limits of Three Liquid Hydrocarbon Fuels Having High Volumetric Energy Content in a J33 Single Combustion
Author: Edward G. Stricker
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 28
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.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 28
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.
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 382
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 382
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 506
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 506
Book Description
Performance Comparisons of JFC-2 and MIL-F-5624A (JP-3) Fuels in Tubular and Annular Combustors
Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 28
Book Description
NASA Technical Note
Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
Book Description
Turbojet Combustor Performance with Natural Gas Fuel
Author: Nicholas R. Marchionna
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description