Title of article
Stability rating tests for the length-optimization of baffles in a liquid propellant combustion chamber using a pulse gun
Author/Authors
Kim، نويسنده , , Hong Jip and Seo، نويسنده , , Seonghyeon and Lee، نويسنده , , Kwang Jin and Han، نويسنده , , Yeoung Min and Lee، نويسنده , , Soo Yong and Ko، نويسنده , , Young Sung، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2008
Pages
9
From page
214
To page
222
Abstract
Stability rating tests using a pulse gun, one type of artificial disturbance device, have been performed to optimize and to limit the axial baffle length of a combustor. To determine whether the combustor is stable when it is exposed to strong external perturbations or pressure oscillations, the decay time and amplitude ratio have been analyzed to quantify the stabilization capacity of the combustor. A baffle not big enough to cover the flame zone considered as the collision plane of the F-O-O-F impinging injector was not able to suppress external perturbations sufficiently. The combustion stability boundary limit of the present combustor can be determined with respect to the axial baffle length.
Keywords
Dynamic stability boundary , Combustion instabilities , Stability rating test , F-O-O-F impinging injector , Pulse gun , Baffle , Decay time , decay rate , Amplitude ratio
Journal title
Aerospace Science and Technology
Serial Year
2008
Journal title
Aerospace Science and Technology
Record number
2229745
Link To Document