Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
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
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
NASA Technical Note
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.
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
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
A Selected Listing of NASA Scientific and Technical Reports for ...
Effects of Fuel-nozzle Carbon Deposition on Combustion Efficiency of Single Tubular-type, Reverse-flow Turbojet Combustor at Simulated Altitude Conditions
Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Carbon
Languages : en
Pages : 34
Book Description
A study was made to determine the cause of irreproducibility of combustion data of a single tubular-type turbojet combustor operating at simulated altitude conditions.
Publisher:
ISBN:
Category : Carbon
Languages : en
Pages : 34
Book Description
A study was made to determine the cause of irreproducibility of combustion data of a single tubular-type turbojet combustor operating at simulated altitude conditions.
Aeronautical Engineering Index
High-altitude Performance of 9.5-inch-diameter Tubular Experimental Combustor with Fuel Staging
Author: Wilfred E. Scull
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64
Book Description