๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Combustion Performance of Gas Turbine Combustors Burning Alternative Fuels

โœ Scribed by Ballal, D.R.; Lefebvre, A.H.


Book ID
120413205
Publisher
American Institute of Aeronautics and Astronautics
Year
1979
Weight
527 KB
Volume
3
Category
Article
ISSN
0146-0412

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Effects of spray characteristics on comb
โœ A. Datta; S. K. Som ๐Ÿ“‚ Article ๐Ÿ“… 1999 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 146 KB ๐Ÿ‘ 2 views

Spray characteristics like mean drop diameter and spray cone angle play an important role in the process of combustion within a gas turbine combustor. In order to study their effects on wall and exit temperature distributions and combustion efficiency in the combustor, a numerical model of a typical

Transient performance of catalytic combu
โœ T. Ahn; W.V. Pinczewski; D.L. Trimm ๐Ÿ“‚ Article ๐Ÿ“… 1986 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 977 KB

The transient response of a monolith catalytic combustor to changes in operating conditions and monolith design parameters has been examined on the basis of a mathematical model. The model considers both catalytic and gas phase reactions and allows for axial conduction of heat in the solid substrate