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
Categorie Soggetti
Aerospace Engineering & Tecnology
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.