An experimental analysis of the precessing vortex core (PVC) instability in a free swirling jet
of air at ambient pressure and temperature is performed by means of laser Doppler …

The present study assesses RANS-based turbulence models to simulate isothermal flow in a
combustor representing a constituent can combustor of can-annular configuration used in jet …

The present study assesses RANS-based turbulence models to simulate the isothermal
confined swirling flow in a combustor representing a constituent can combustor of the can …

three dimensional numerical investigation of the combustion of methane air mixture in gas
turbine Can-combustor by using CFD with CFX solver is presented in this study. The …

A complementary experimental and computational study of the flow and mixing in a single
annular gas turbine combustor has been carried out. The object of the investigation is a …

This paper presents a study of the flow patterns typical of “Rich-burn, Quick-quench, Lean
burn”, RQL, gas-turbine combustors based on detailed velocity measurements of the flow in …

The annulus flow characteristics of a can-combustor model for different liner dome shapes
have been experimentally established under isothermal flow conditions for both nonswirling …

A three-dimensional numerical study was performed to assess the effects of inlet
temperature and equivalence ratio on the spray combustion and subsequent NOx emission …

The measurements of mean and turbulent quantities presented in Part 1 showed a strong
influence of the primary jet system and evidence of the existence of bimodal distributions of …

A method for characterizing the flowfield associated with an ensemble of production swirl
cups before their implementation into an aircraft engine is presented. LDV is used to acquire …