| || Velocity Distribution in the Annuli of a Plane Reverse Flow Combustor Model
Author : Bharani, Sanjeev;Singh, S.N.;Agrawal, D.P.
Source : Defence Science Journal ; Vol:50(2) ; 2000 ; pp 137-146
Subject : 629.7 Aeronautics
Keywords : Flow distribution;Reverse flow gas turbine combustor;Inlet flow velocity.
Abstract : "This paper reports the velocity profiles and flow distribution in the annuli of a plane reverse-flow gas turbine combustor model. Based on these, flow-split through different liner holes and swirlers has been estimated. It is seen that percentage flow-split through the outer liner surface holes, compared to that through liner dome and inner liner surface holes, is not affected significantly by increase in the inlet flow velocity. "