Some of the significant achievements of the National Programme – Gas Turbine Enabling Technology (GATET) (2009-2017) formulated by GTRE and AR&DB Propulsion Panel are as follows.
1. Design Tools, Software, Simulation Models & Methodologies – Bond Graph Technique for Damper Design, DNS & LES based CFD codes, Aero-acoustics etc., (25 No’s)
•Development of Direct Numerical Simulation (LES) Code through JNCASR, Bangalore to Analyze Flow& Heat Transfer through Turbo-machinery Blades.
Development of Large Eddy Simulation (LES) Code through IISc, Bangalore to Analyze Flow through Turbo-machinery Blades.
Development of Acoustic Analysis Method for Afterburner Screech Liner through IIT Hyderabad.
Reduced Order Bond Graph Method for Designing Floating Mass Dampers through IIT Kharagpur.
Studies on Improving Axial Flow Compressor Performance through IIT Madras.
2. Experimental Facilities & Infrastructure– Flutter, Screech, Squeeze Film Dampers & InterShaft Bearings etc., (10 Nos.)
 Facility Established at NAL, Bangalore to Understand Afterburner Screech
 Facility Established at IISc, Bangalore to Understand Transonic Stall Flutter
 Test Rig for Characterizing Inter Shaft Bearings Established at NAL, Bangalore
 High Speed Bearing Test Facility Established at Veltech University, Chennai
 Test Rig Established at IIT Kanpur for Studying Aero-Elasticity of Turbo-machinery Blades.
3. Design Verification & Validation Tests on Engine Components & Models – Compressor & Turbine maps of STFE, Correlations & Test Data for Cooling Turbine Blades & Combustor
Liners (12)
 Rotating Test Rig Established at IIT Bombay for Blade Cooling Experiments
Spray Patternation Test Stand Established at GTRE through IIT Madras for Characterizing Atomisers
Matrix Cooling Test Rig Established at IIT Roorkee
Impedance Tube Facility Established at IIT Dhanbad for Acoustical Measurements
Experimental Characterization of STFE Turbine & Compressor at NAL, Bangalore through Facility Upgradation
Experimental Data Generation pertinent to Effusion Cooling of Combustor Liner through NAL, Bangalore.
4. Futuristic Technologies – Active Magnetic Bearings (AMB), Inter-Pulse TIG welding, Metal Matrix Composites, Multi Variable Control etc., (16 Nos.)
AMB Developed through NAL, Bangalore
Gas Turbine Research Laboratory (Engine Controls) Established at IIT Bombay
IPTIG Welding Process Developed through Annamalai University (IPTIG Machine Handed Over to GTRE)
5. Product & Process Development – Sensors (Thin Film based for Strain, MEMS based for Vibration, Inductive Pulse based for Oil Debris Detection), JP10 Synthesis (lab scale) etc., (6 Nos.)
In summary, the achievements made through GATET initiative played a vital role in the indigenous design, development and realization of gas turbine engines and their components for the current & future engine programs in the country.
Some of the significant achievements of the Propulsion Panel projects from 2018-2023 are as follows:
Investigation on Spray Combustion Characteristics of JP-10 Embedded with Boron Particles. Useful for Future Small Gas Turbine Engine Programmes of GTRE
Development Studies on 50N Thrust Class Liquid Fueled Valveless Pulsejet Engines. Useful for Indigenous expendable propulsion system for MAVs and target drones of ADE
Dynamic Data Driven Control for Mitigation of Lean Blow out Gas Turbine Combustors. Domain Lab/Probable Beneficiary: GTRE/DRDL
Synthesis of Potential High Energy Density Fuels: An Alternative to JP-10 Fuel for Air-breathing Missiles. Domain Lab/Probable Beneficiary: DRDL/GTRE
Design of an Integral Squeeze Film Damper (SFD). Domain Lab/Probable Beneficiary: GTRE/DRDL
Preparation of Air-Stable and Hydro Carbon Fuel Dispersible Amorphous Nano-boron Powder for Solid Rocket Motor and Air Breathing Missile Application. Domain Lab/Probable Beneficiary: DRDL
Experimental Investigation of Primary and Secondary Breakup of Liquid Jets in Coaxial Air-Blast Atomisation. Domain Lab/Probable Beneficiary: GTRE