ACTIVE CONTROL OF TWIN-PULSE COMBUSTORS

Citation
M. Zeutzius et al., ACTIVE CONTROL OF TWIN-PULSE COMBUSTORS, AIAA journal, 36(5), 1998, pp. 823-829
Citations number
14
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00011452
Volume
36
Issue
5
Year of publication
1998
Pages
823 - 829
Database
ISI
SICI code
0001-1452(1998)36:5<823:ACOTC>2.0.ZU;2-Z
Abstract
The pressure losses of steady-flow combustors can be overcome with so- called pressure gain or pulse combustors. Higher combustion efficiency and low NO, are the well-known advantages that outweigh the disadvant ages of noise, combustor control, and lower operational flexibility. I nlets with variable cross section enable an active control of the comb ustor as gas generator for turbines. Therefore, a special emphasis is given to the design of the inlet, its control capacity, and its impact on combustor and turbine performance.