NUMERICAL AND EXPERIMENTAL INVESTIGATION OF FLOW IN AN AFTERBURNER
By Suresh Kumar S (ME02S004)
Project Objective…
Optimization of flame stabilizer location in an aero engine gas turbine afterburner w.r.t. flame stabilizer. Experimental investigation of flow in a model afterburner and comparison of results with the code.
Schematic Diagram of an Afterburner
Struts
Fuel Manifolds
Pre-Diffuser
Screech Holes
V-Gutter
Cooling Rings
Variable nozzle
1800 Sector of an Afterburner
1800 Section of a V-Gutter
Geometry Creation goes in this way..
The geometry was created using the modeling software named CATIA.
Geometry Creation(Contd..)
Geometry Creation(Contd..)
Geometry Creation(Contd..)
Geometry Creation(Contd..)
Geometry Creation(Contd..)
Geometry Creation(Contd..)
Geometry Creation(Contd..)
Geometry Creation(Contd..)
Surface mesh of a 1800 Sector Afterburner
Model in CATIA ( 90 Degree Sector)
Model Geometry Contd..
Mesh in Gambit
1220489 Cell Size
Work done so far..
Axial velocity vectors in the mid-plane