Suresh After Burner

  • November 2019
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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

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