Author : Stephen C. Harding
Publisher :
Page : 0 pages
File Size : 48,60 MB
Release : 1998
Category :
ISBN :
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, Jun 2-Jun 5, 1998.
Author :
Publisher :
Page : 974 pages
File Size : 46,22 MB
Release : 1999
Category : Aeronautics
ISBN :
Author : J. M. Deur
Publisher :
Page : 18 pages
File Size : 35,8 MB
Release : 1995
Category : Air
ISBN :
Author : Arnaud Lacarelle
Publisher : Univerlagtuberlin
Page : 317 pages
File Size : 28,81 MB
Release : 2011
Category :
ISBN : 9783798323810
Author :
Publisher :
Page : 18 pages
File Size : 15,11 MB
Release : 1993
Category :
ISBN :
Author : Johannes W. Koopman
Publisher :
Page : 0 pages
File Size : 30,91 MB
Release : 1998
Category :
ISBN :
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, June 2 - June 5, 1998.
Author : Robert C. Steele
Publisher :
Page : 0 pages
File Size : 19,93 MB
Release : 1999
Category :
ISBN :
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Indianapolis, Indiana, June 7-June 10, 1999.
Author : Andrei Lipatnikov
Publisher : CRC Press
Page : 548 pages
File Size : 36,26 MB
Release : 2012-10-24
Category : Science
ISBN : 1466510250
Lean burning of premixed gases is considered to be a promising combustion technology for future clean and highly efficient gas turbine combustors. Yet researchers face several challenges in dealing with premixed turbulent combustion, from its nonlinear multiscale nature and the impact of local phenomena to the multitude of competing models. Filling
Author :
Publisher :
Page : 50 pages
File Size : 41,87 MB
Release : 1977
Category :
ISBN :
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 82 pages
File Size : 42,18 MB
Release : 2018-05-29
Category :
ISBN : 9781720461401
NO(x) reduction is a driving force in combustor design today. The fuel-air mixing process can have a significant effect on NO(x) production. This report describes a set of experiments carried out to assess fuel-air mixing sensitivities to geometric variation in the Rich-Burn/Quick-Mix/Lean-Burn (RQL) combustor concept utilized in stationary gas turbine engine applications and proposed for advanced transport aircraft engines. Specifically, three (3) parameters in the quick-mix zone were examined: jet injection angle, jet-to-expansion distance, and jet count (number of jets).Samuelsen, G. S. and St.John, D.Glenn Research CenterNITROGEN OXIDES; GAS TURBINE ENGINES; JET FLOW; INJECTION; GAS EXPANSION; COMBUSTION CHAMBERS; AIRCRAFT ENGINES
