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- Development of Fluidic Thrust Vectoring Capability for AURA High Aspect Ratio Fixed Nozzle (ADA)
- Application of Bio-Fuels for Aviation (DST + PWC): Indian partners: IIP, IISc, IOCL, HPCL, Infotech
- Passive and Active Control of Hooting (Pratt and Whitney, Canada)
- HIGH SPEED WIND TUNNEL TESTING OF 120MM FSAPDS Mk II AMMUNITION (ARDE/DRDO)
- Experimental Investigation of Flow Separation in Proposed AURA intake duct and its control (ADA)
- Development of a Morphing Wing (DRDO)
- Study of Internal Flow Dynamics in a 2D Curved Nozzle and Development of Fluidic Thrust Vectored Nozzle (AR&DB)
- Development of Test Facility for Fire Propagation and Associated Thermal Hydraulic Aspects in Multiple Compartments (BARC)
- Study of spray combustion in a swirl stabilized dump combustor (ISRO-STC)
- Identification and Control of Combustion Instability in Bluff Body Stabilized diffusion flame (ISRO-STC)
- Development of a Hybrid Pulsed Plasma Thruster (ISRO-STC)
- Experimental Study of Aeroelastic behaviour of cascades (AR&DB)
- Identification Analysis and Control of Flow Angularity in Thrust Vectored Nozzles (AR&DB)
- Aerodynamic Characterization of Projectiles with Wrap Around Fins (ARMREB)
- Flow Control in Serpentine Intakes using Pulsed Vortex Generator Jets (AR&DB)
- Droplet-Flow Interaction in Re-circulating Turbulent Flows (ISRO-STC)
- Development of “Smart” Vortex Generators for prevention of flow separation and enhancement of stall margin for airfoil sections (ADA)
- Study of Liquid Fuel Combustion in a Re-circulating Flow Field of Gaseous Oxidizer. (ISRO-STC)
- Up gradation of Tri-Sonic Wind Tunnel at IIT Kanpur for Testing of Armament Stores. (ARMREB)
- Solution of HPT-32 engine cut-off problem (CEMILAC, RCMA, DRDO)
- Design and Modeling of Liquid Atomizers (CFEES, DRDO)
- Modeling of Fire-Water Mist interactions in enclosures (CFEES, DRDO)