-
Studies of Fire Propagation, Suppression and Scavenging with Associated Thermal Hydraulic Aspects in Multiple Compartment (BARC)
-
Data for jets and sprays in cross flow (Pratt and Whitney, USA)
-
Characterization and Fluidic Thrust Vector Control of GHATAK elliptic Nozzle model fitted to a miniature gas turbine engine (ADA)
-
Characterization and Simulation of the performance of Twin-Fluid Atomizers (HPCL)
-
GO2/GCH4 Combustion Studies In High Pressure Rocket Combustors (ISRO/STC)
-
Aerodynamic Characterization of Projectiles with Wrap Around Fins (ARMREB)
-
Design and Development of Single Fluid Atomizers for Mist Generation (CFEES, DRDO)
-
Aero-elastic study of Turbo-machinery blades (GATET, DRDO)
-
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)
-
Experimental Investigation of Flow Separation in Proposed AURA intake duct and its control (ADA)
-
Development of a Morphing Wing (DRDO)
-
Development of Test Facility for Fire Propagation and Associated Thermal Hydraulic Aspects in Multiple Compartments (BARC)
-
Study of Internal Flow Dynamics in a 2D Curved Nozzle and Development of Fluidic Thrust Vectored Nozzle (AR&DB)
-
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)
High Speed Wind Tunnel Testing of 120 mm FSAPDS Mk II Ammunition (ARDE/DRDO)