Title
Effect Of Different Annulus Heights On Performance Of Annular Gas Turbine Model Combustor
Abstract
Present study is a numerical investigation on an annular gas turbine combustor model with the simulation of dump diffuser and annuli. Uniform pressure distribution around the liner is desired for designed flow-split through the liner holes. An attempt has been made to achieve uniform velocity and pressure conditions in the annuli (around the liner) by changing the annuli height thereby changing the outer annulus area to-inner annulus area ratio. It is found that for the area ratio of 2.56, uniform velocity and constant pressure condition is achieved around the bluff body representing the liner in the combustor model.
Publication Date
12-1-2002
Publication Title
Indian Journal of Engineering and Materials Sciences
Volume
9
Issue
6
Number of Pages
403-408
Document Type
Article
Personal Identifier
scopus
Copyright Status
Unknown
Socpus ID
0036993639 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/0036993639
STARS Citation
Garg, Gourav; Bharani, Sanjeev; and Singh, S. N., "Effect Of Different Annulus Heights On Performance Of Annular Gas Turbine Model Combustor" (2002). Scopus Export 2000s. 2343.
https://stars.library.ucf.edu/scopus2000/2343