NATIONAL CONFERENCE ON WIND TUNNEL TESTING(NCWT-05)
Jointly organized by
Anna University, Madras Institute of Technology Campus and CSIR-SERC, Chennai
16-17 March 2017, Venue : Rajam Hall, MIT Campus, Chrompet, Chennai-44
Anna University, Madras Institute of Technology Campus and CSIR-SERC, Chennai
16-17 March 2017, Venue : Rajam Hall, MIT Campus, Chrompet, Chennai-44
Partial List of Accepted Papers for Oral Presentation as on 10.02.2017. This list will be updated soon.
| Aerodynamic Characteristics of an Aerospace Vehicle with Side Mounted Air-Intake in Closed Condition at Subsonic and Supersonic Flow | DRDL, Hyderabad | ||
|---|---|---|---|
| Design and Fabrication of Compact Mass Flow Controller Device to Suit 60 mm Mass Flow Duct | NAL, Bengaluru | ||
| Automation of Load Application by Pneumatic/ Hydraulic Systems on Wind Tunnel Balance | NAL and University Visvesvaraya College of Engineering, Bengaluru | ||
| Theoretical and Experimental Evaluation of Propeller Thrust with Respect to Freestream Velocity and RPM for a MAV | MIT, Chennai | ||
| Development of Cowl Actiation Mechanism of an Air-Intake Model | NAL & Central Manufacturing Technology Institute, Bengaluru | ||
| Application of Global Regression Method for Calibration of Hinge Moment Balances | NAL, Bengaluru | ||
| Check Calibration Tests for Force and Moment Measurements in Wind Tunnels at NTAF | NAL, Bengaluru | ||
| Investigation of Flow Over a Cone-Cylinder at High Angles of Attack at Subsonic Speed | BIT, Ranchi | ||
| Base Drag Reduction Studies by Experiment and CFD at Low Speeds | KCG college of Technology, Chennai & DRDL, Hyderabad | ||
| Anhedral Angle Effect on a 76/40 Degree Double Delta Wing at Subsonic Speed | BIT, Ranchi | ||
| Design and Development of a Rig for Calibration of Balances with High Axial Load Capacity | NAL, Bengaluru | ||
| Design of Support Systems for Full Scale Fin Model for Force and Moment Measurements in 1.2 m Wind Tunnel | NAL, Bengaluru | ||
| Design Optimization and Analysis of a Turbo-Ramjet Diffuser | MIT, Chennai | ||
| Experimental Investigation on Induced Drag Reduction on Aircraft Model with Winglet | Rajalakshmi Engineering college and MIT, Chennai | ||
| Model to Sting Annular Gap Estimation- An Experimental Investigation | NAL, Bengaluru | ||
| LabVIEW Based Data Reduction Program for Dynamic Derivative Measurements using Free Oscillation Technique | NAL, Bengaluru | ||
| Performance of Air-Intake at Off-Design Mach Number | DRDL, Hyderabad | ||
| Dynamic Measurements of Modal Deflection Using Image Processing | NAL, Bengaluru | ||
| Characterization of Dielectric Barrier Discharge Plasma Actuator for Wind Tunnel Application | NAL & IISc., Bengaluru | ||
| LabVIEW Based Real-Time Mach Analysis System for Trisonic Wind Tunnel | Dr. Ambedkar Institute of Technology & NAL, Bengaluru | ||
| Control System Development for Wind Tunnel and Their Applications | NAL, Bengaluru | ||
| Aerodynamic Characterization of a Typical Anti-Tank Guided Missile with High Aspect Ratio (Hi-AR) Wing Configuration | DRDL, Hyderabad | ||
| Rudder Hinge Moment for Scaled Model of a Generic Winged Body Configuration at Transonic Mach Number | VSSC, Thiruvananthapuram & NAL, Bengaluru | ||
| Development of a New Ejector Eacility in NTAF, CSIR, NAL | NAL, Bengaluru | ||
| Wind Tunnel Study of a Bio-Inspired Corrugated Wing | VFSTR University, Gundur & Narasaraopeta Engineering College, Andhra pradesh | ||
| Effect of Interference on Wind Loads on Rectangular Plan Tall Buildings | IIT-Roorkee | ||
| Effect of Spacing on Wind Pressure Distribution on Flat Canopy Roof | IIT-Roorkee | ||
| Design of a Rectangular-type Hinge Moment Balance for Load Measurements on Control Surfaces of a Missile-type Wind Tunnel Model | NAL, Bengaluru | ||
| Wind Pressure Distribution on Low Rise Buildings with Hip Roof | GBPUA&T, Pantnagar University, and IIT-Roorkee, Uttarakhand | ||
| Hypersonic Aerodynamic Characterization of a Winged Body Configuration at High Angle of Attack | VSSC, Thiruvananthapuram | ||
| Qualification of Thermal Protection System Under Aerodynamic Shear and Heat Load | VSSC, Thiruvananthapuram | ||
| Influence of Corner Configuration on Wind Loads on Tall Buildings | IIT-Roorkee | ||
| Effect of Wind Incidence Angle on Wind Pressure Distribution on Canopy Roofs | IIT-Roorkee | ||
| Experimental Investigation of Wind Loads on High-Rise Buildings | IIT-Roorkee | ||
| Wind Pressure Distribution on Industrial Building Roof | IIT-Roorkee | ||
| Effect of Roof Slope on Wind Pressure Distribution on Conical Roofs | IIT-Roorkee | ||
| Prediction of Supersonic Flow Instability inside an Air-Intake of Combat Aircraft through Wind Tunnel Testing | ADA and NAL, Bengaluru | ||
| Development and Evaluation of Co-axial Thermocouples for Heat Flux Measurements | VSSC, Thiruvananthapuram | ||
| Experimental Setup for Scramjet Combustion Experiments in Short Duration Impulse Facilities | VSSC, Thiruvananthapuram | ||
| Effect of Leading Edge Profile Over the Flow Phenomenon of Delta Wing | Tagore Engineering College and MIT, Chennai | ||
| Effect of Modification of Sharp Base on Base Pressure | NAL, Bengaluru | ||
| Control of Shock Wave Boundary Layer Interaction Using Passive Device Over a Forward-Facing Step | NAL, Bengaluru | ||
| Effect of Modified Nose Cone Shape on the Performance of a Generic Air Vehicle | ADE, Bengaluru | ||
| Experimental Study of the Effect of Wake due to Circular Cylinder | MIT, Chennai and Sastra University, Thanjavur | ||
| Investigation of Steady and Unsteady Flow inside an Air-intake at Supersonic Speed | BIT, Ranchi | ||
| Development of Expanded Jets Through a Linear Cluster Plug Nozzle | NAL, Bengaluru | ||
| Full Scale Wind Tunnel Testing to Estimate the Rudder Hinge Moment of a UAV Vertical Tail | ADE, Bengaluru | ||
| Implementation of Non-Contact Measurement Technique for Aeroelastic Testing in Low Speed Wind Tunnel | NAL, Bengaluru | ||
| Novel Method for Aerodynamic Shear Simulation on a Subscale Tank Filled with Cryo Fluid | VSSC, Thiruvananthapuram | ||
| Vortex Induced Vibrations of a Bridge: Effect of Porosity of Railings | IIT, Kanpur | ||
| Experimental Investigations of a Flow Past a Bluff Body | IIT, Kanpur | ||
| Evolution of Payload Faring Nose Configuration for a Typical Space Vehicle | VSSC, Thiruvananthapuram & NAL, Bengaluru | ||
| Alleviation of Core Nozzle Loads for a Booster Assisted Launch Vehicles | VSSC, Thiruvananthapuram, SCL, Department of Space, Punjab & NAL, Bengaluru | ||
| Experimental and Numerical Studies on Propeller Characteristics | Kumaraguru College of Technology, Coimbatore & MIT, Chennai | ||
| Experimental Determination of Heat Transfer in the Wake Region of Reentry Capsule in Plasma Wind Tunnel Facility | VSSC, Thiruvananthapuram | ||
| Experimental and Computational Estimation of an Aerodynamic Characteristic of a Missile Configuration | Amity University, Uttar Pradesh | ||
| Aero-Acoustic Distribution on a Typical Launch Vehicle Stringers at Mach 2 | VSSC, Thiruvananthapuram | ||
| Conjugate Heat Transfer Analysis of Mach 8.0 Nozzle for Hypersonic Wind Tunnel | DRDL, Hyderabad | ||
| Aerodynamic Study on Randome Structure Mounted on Top of a Surveillance Aircraft | CABS, DRDO and IIAEM, Bengaluru | ||
| Scramjet Combustion Experiments in 1m Shock Tunnel | VSSC, Thiruvananthapuram | ||
| Experimental Investigation of Clap and Fling Type Flapping Mechanism with Two Wings and Four Wings | CSIR-NAL, Bengaluru & NALTECH, Bengaluru | ||
| Experimental Investigation of a Powered-on Full Scale Fixed Wing MAV at MART Facility and Validation Through Flight Tests | CSIR-NAL, Bengaluru | ||
| Validation of Complimentary Filter Algorithm for Angle of Attack Estimation using wind tunnel Measurements | SASTRA University, CSIR-NAL & NALTECH | ||
| Experimental Study: Effect of Slider Reefing on Opening Shock Force and Aerodynamic Characteristics of Square Canopy Parachute | ADRDE, Agra | ||
| Automatic Dust Removal System on a Car | Bannari Amman Institute of Technology, Sathyamangalam & MIT, Chennai | ||
| Flow Analysis over Low Rise buildings | Bannari Amman Institute of Technology, Sathyamangalam & MIT, Chennai | ||
| Pressure and Heat Flux Estimation of Hypersonic Cruise Vehicle Using CFD and Shock Tunnel | DRDL, Hyderabad | ||
| Force Measurement on Heat Shield Panels during Separation at Hypersonic Mach Number | DRDL, Hyderabad and IISc., Bengaluru | ||
| Design of a Wind Tunnel Model for Measuring Base Drag in a Supersonic Flow | Excel Engineering College Namakkal, DRDL & RCI Hyderabad | ||
| Hydrodynamic Testing of Different Parachutes in Tow Tunnel for Performance Characterization | ADRDE, Agra | ||
| Wind Tunnel Test results of Parachutes Configured with Reefing Line | ADRDE, Agra & IIT Kanpur | ||
| Wind Tunnel Pressure Measurement Studies on a Model of Photovoltaic Panel with Reflectors | CSIR-SERC, Chennai | ||
| Effect of Wind Tunnel Wall Blockage, Interference Effect and Local Flow Angle Change on Rudder Hinge Moment Characteristics | ADE, Bengaluru | ||
| Effect of Geometry of Cone on Drag and Flow Field of Bluff Body Model | MIT, Chennai & Kumaraguru College of Technology, Coimbatore | ||
| Aerodynamic Design of Flying Wing MAV with Moving Wings | MIT, Chennai | ||
| Wind Pressure Coefficient of Curved Roof Structures: a Comparison Between Wind Tunnel Experiments and Numerical Simulations | SERC, Chennai | ||
| Design and Fabrication of Alpha-Beta Vane for Small UAV Application | IIT, Kharagpur | ||
| Calibration of Single Componenet Accelerometer Force Balance and vibrometer balance using short Duration step load | NIT, Meghalaya & IIT, Guwahati | ||
| Aerodynamic coefficients of a Model of a Curved Transitory Shelter Under Simulated Wind | CSIR-SERC, Chennai & R&DE(E), Pune |