Investigation of Altitude Performance of AN-F-58 Fuels in Annular Combustor of J34-WE-22 Engine PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Investigation of Altitude Performance of AN-F-58 Fuels in Annular Combustor of J34-WE-22 Engine PDF full book. Access full book title Investigation of Altitude Performance of AN-F-58 Fuels in Annular Combustor of J34-WE-22 Engine by Adelbert O. Tischler. Download full books in PDF and EPUB format.
Author: Adelbert O. Tischler
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 35
Get Book Here
Book Description
Author: Adelbert O. Tischler
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 35
Get Book Here
Book Description
Author: Adelbert O. Tischler
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 90
Get Book Here
Book Description
Author: Eugene V. Zettle
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 44
Get Book Here
Book Description
Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 23
Get Book Here
Book Description
Three fuels conforming to AN-F-58 specification were investigated in order to determine the influence of boiling temperatures and aromatic content on altitude performance in single combustor of a 4600-pound-thrust turbojet engine. Combustion efficiencies of the three AN-F-58 fuels were approximately equal at each simulated engine condition for altitudes from 5,000 to 50,000 feet, 90-percent normal rated engine speed, and flight Mach numbers of 0.0 and 0.6.
Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 28
Get Book Here
Book Description
Author: Edward G. Stricker
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 28
Get Book Here
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: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
Get Book Here
Book Description
Author: RIchard J. McCafferty
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 96
Get Book Here
Book Description
Author: James L. Jr Harp
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Get Book Here
Book Description
