Turbojet Combustor Performance with Natural Gas Fuel
Author : Nicholas R. Marchionna
Publisher :
Page : 44 pages
File Size : 36,26 MB
Release : 1970
Category : Airplanes
ISBN :
Author : Nicholas R. Marchionna
Publisher :
Page : 44 pages
File Size : 36,26 MB
Release : 1970
Category : Airplanes
ISBN :
Author : James S. Fear
Publisher :
Page : 28 pages
File Size : 29,21 MB
Release : 1970
Category : Airplanes
ISBN :
Combustion efficiency was determined using natural gas fuel over a range of injection temperatures from ambient to 1200' F (922 K). The combustor was comprised of three U-gutter flameholders mounted downstream of a trumpet-shaped diffuser in a rectangulai housing. A simple film-cooled liner was used. Tests were conducted at ambient pressure over a range of fuel-air ratios and combustor reference velocities. Increases in efficiency of more than 40 percentage points were achieved at the higher fuel temperatures. The results are applicable to natural gas afterburner design and to the design of advanced low-pressure-loss primary combustors.
Author : Nicholas R. Marchionna
Publisher :
Page : 33 pages
File Size : 19,10 MB
Release : 1970
Category : Airplanes
ISBN :
Author : Nicholas R. Marchionna
Publisher :
Page : 38 pages
File Size : 25,52 MB
Release : 1970
Category : Airplanes
ISBN :
Author : James S. Fear
Publisher :
Page : 20 pages
File Size : 47,53 MB
Release : 1970
Category :
ISBN :
Author : James S. Fear
Publisher :
Page : 19 pages
File Size : 26,78 MB
Release : 1970
Category : Airplanes
ISBN :
Combustion efficiency was determined using natural gas fuel over a range of injection temperatures from ambient to 1200' F (922 K). The combustor was comprised of three U-gutter flameholders mounted downstream of a trumpet-shaped diffuser in a rectangulai housing. A simple film-cooled liner was used. Tests were conducted at ambient pressure over a range of fuel-air ratios and combustor reference velocities. Increases in efficiency of more than 40 percentage points were achieved at the higher fuel temperatures. The results are applicable to natural gas afterburner design and to the design of advanced low-pressure-loss primary combustors.
Author : James S. Fear
Publisher :
Page : 0 pages
File Size : 39,31 MB
Release : 1970
Category : Airplanes
ISBN :
Author : Helmut F. Butze
Publisher :
Page : 50 pages
File Size : 31,33 MB
Release : 1979
Category : Airplanes
ISBN :
Author : Philip P. Walsh
Publisher : John Wiley & Sons
Page : 664 pages
File Size : 18,72 MB
Release : 2008-04-15
Category : Technology & Engineering
ISBN : 140515103X
A significant addition to the literature on gas turbine technology, the second edition of Gas Turbine Performance is a lengthy text covering product advances and technological developments. Including extensive figures, charts, tables and formulae, this book will interest everyone concerned with gas turbine technology, whether they are designers, marketing staff or users.
Author : Allen J. Metzler
Publisher :
Page : 42 pages
File Size : 44,12 MB
Release : 1956
Category : Airplanes
ISBN :