Industrial Consultancy & Sponsored Research (IC&SR) , IIT Madras
Aerospace & Defense Technologies
- IDF No 1129 Hybrid Rocket Engine Having High Regression Rate
- IDF No 1327 Floating Wiper Inductive Voltage Divider Type Displacement Transducer
- IDF No 1350 Swirl Number Selection for Reduction of Various Forms of Jet Noise
- IDF No 1946 Systems and methods for suppressing thermo-acoustic instabilities in a Combustor
- IDF No 2446 Metallic Functionally Graded Materials and Manufacturing Methods thereof
- IDF No 2428 Solar Array for a Rotatable Object
- IDF No 1383 Anti Air Column Interaction Mounting for Multirotor Aerial Vehicles
- IDF No 1327 Floating Wiper Inductive Voltage Divider Type Displacement Transducer
- IDF No 1350 Swirl Number Selection for Reduction of Various Forms of Jet Noise
- IDF No 1598 A Jet Impingement Cooling System with Improved Showerhead Arrangement for Gas Turbine Blades
- IDF No 2329 Linear Induction Motor with Reduced End-effects
- IDF No 1537 Multi-rotor Aerial Vehicle with Variable Center of Gravity and Method Control thereof
- IDF No 1965 A Lift Separation Sabot for Kinetic Energy Projectiles
- IDF No 1900 Two-stage Design Based High Speed Gas Gun
- IDF No 2107 Cooling intricate parts with an additive wall mounted pressurized spray/jet
- IDF No 1350 Swirl Number Selection for Reduction of Various Forms of Jet Noise
- IDF No 1325 High Strain Rate Tensile Testing Set-up by Impact Loading
- IDF No 1666 An Air Swirler Fuel Atomizer Assembly with Variable Hub to Tip Aspect Ratio
- IDF No 1665 A Rotating Spindle Type Fluid Atomizer for Spray Atomization
- IDF No 1349 Structural Frame for Impingement Noise Reduction
- IDF No 1736 Hybrid Wing Device and Method of Actuation
- IDF No 1236 A Multirotor with a Vertically Offset Overlapping Configuration and Uses thereof
- IDF No 2336 External Attachment to Increase Aerodynamic Efficiency of a Wing Applicable for Aeroplanes, Turbines and Fans
- IDF No 1977 Determining Onset of Combustion Instability in a Combustion System
- IDF No 1210 System and Method for Generating Precursors for Early Detection of Impending Aeroelastic Instabilities