CFD Final papers
P1-EFFECT OF TRAILING EDGE REFINEMENT ON FORCE CONVERGENCE AND ACCURACY FOR FLOW OVER BLUNT TRAILING EDGE AIRFOIL
P2-Adjoint based Sensitivity Analysis for Navier-Stokes Equations
P3-ANALYSIS OF MULTI ROW DISK INLET DEVICE IN SUPERSONIC FLOW CONDITION
P4-COMPUTATIONAL AND EXPERIMENTAL INVESTIGATION OF SUBSONIC FLOW OVER A SAWTOOTH NOTCHED DELTA WING-AMITY
P5-Numerical and Experimental Investigation of Blended Wing Body Configuration
P6-PERFORMANCE ANALYSIS OF CONICAL SCARFED NOZZLES USING CFD-IIST
P7-Computational Analysis of Shock Wave Boundary Layer Interaction using Shock Impingement Method
P8-LES SIMULATION OF SCREECH COMBUSTION INSTABILITY IN A MODEL AERO-GAS TURBINE AFTERBURNER
P9-Numerical study on the effects of conical angle on the performance of a vortex tube
P10-Mechanism of vortex asymmetry over Slender Body at High angle of attack
P11-NUMERICAL SIMULATION OF STORE SEPERATION USING DIFFERENT MESH TYPES IN OVERSET MESHING APPROACH
P12- Numerical Study of swirling flows
P14-DESIGN OPTIMISATION OF FRONT WING OF A FSAE RACE CAR USING CFD
P15-Modeling aerodynamics for ultra-low Reynolds Number flight
P16-SONIC BOOM MINIMIZATION IN CONCEPTUAL DESIGN - IIT-Bombay
P17-Improved Efficient Modeling of Gust Flow Over Flying Configurations Using Overset Mesh Approach
P18-Design and CFD Analysis of a Multi Stage Axial Flow Compressor
P19-Numerical Simulations of Wing Deployment Using Overset Grid Technique-ADE (2)
P20-GPU Accelerated Meshfree Solvers for Compressible Flows-BITS-Hyderabad (2)
P21-Numerical Investigation of Ground Effect on Aerodynamics of Winged Body Re-entry Configuration-VSSC1 (1)
P22-Implementation and application of AUSM+ -up and AUSM+ -up2 schemes in open-source CFD code SU2
P23-NUMERICAL SIMULATION OF HYDROGEN COMBUSTION IN GENERIC SCRAMJET COMBUSTOR-VSSC3
P24-Effect of stringer on overall aerodynamic coefficient of a typical launch vehicle-VSSC4
P25-Aerodynamic characterization of a typical launch vehicle with two strapons-VSSC5
P26-Venting Performance of a Typical Payload Fairing Using Transient CFD APPROACH-VSSC6
P27-Performance Enhancement of an Immersed Boundary Method Based FSI Solver Using OpenMP
P28-Reconstruction of Flows using Convolutional neural networks-IITM
P29-AERODYNAMIC SHAPING OF A CREW ESCAPE SYSTEM – AXISYMMETRIC ANALYSIS
P30-Numerical Analysis of Wing-Tip Mounted Propeller Interaction using Actuator Disk Model-Siemens
P31-Aerodynamic Shaping of Base Region of a Multi-Body Launch Vehicle
P32-USE OF CFD AS A REACTIVE TOOL TO ADDRESS ENGINE COMPARTMENT OVERHEATING PROBLEMS IN A MILITARY COMBAT/ TACTICAL VEHICLE
P33-MITIGATION OF SLOSHING IN AN UPRIGHT CIRCULAR CYLINDRICAL ROCKET PROPELLANT TANK BY A FLOATING BAFFLE
P34-ADVERSE EFFECT OF PLUME IMPINGEMENT ON THE THERMALLY PROTECTIVE DIAPHRAGM OF A ROCKET LAUNCHER POD
P35-Numerical Investigation of the Flow Past 6 1 Prolate Spheroid
P36-ANSYS_Scale-Resolving-Simulation-of-Launch-Vehicle-at-Transonic-Speed
P37-Sensitivity analysis and optimization of a trainer aircraft configuration using open source tool SU2
P38-Numerical Simulation of Transitional Flow Past SD7003 Airfoil over a Range of Reynolds Number
P39-Rudder Deflection Studies On SARAS Using Mesh-Free Solver-CTFD4
P40-COMPUTATIONAL STUDY OF AERODYNAMIC CHARACTERISTICS OF A PROJECTILE BY VARYING BOAT TAIL CONFIGURATION
P41-ANSYS-Mosaic-Poly-Hexcore-Mesh-For-High-Lift-Aircraft-Configuration
P42-CFD Analysis on Preliminary Layout of 2.5 m Continuous Wind Tunnel
P43-NUMERICAL INVESTIGATION OF THE POINT-IMPLICIT SCHEME FOR THE 1-D HEAT EQUATION.
P46-INVESTIGATIONS ON THE SHAPE OPTIMIZATION OF NACA0012 IN GROUND EFFECT
P47-Effect of Asymmetric Propeller Thrust on Aircraft with Rudder Deflection A CFD Perspective
P48-SIMULATION OF DEFORMATION OF AN ELASTIC CAPSULE IN FLUID FLOW USING IMMERSED BOUNDARY METHOD-NITK (2)
P49-SIMULATION OF SCRAMJET COMBUSTOR USING QUASI 1-D AND 3-D CFD MODELS-DRDL1 (2)
P50-Effect of Vortex Generators on the Vertical tail of SARAS PT1N Aircraft-CTFD7 (2)
P51-Euler Studies on 21463 RTA-70 configuration using Hyena-CTFD8 (2)
P52-Numerical Analysis of Aerodynamic Characteristics of a Corrugated MAV wing.
P53-Numerical simulation of wind flow and heat transfer over a cluster of buildings
P54-GLOBAL SPECTRAL ANALYSIS FOR CONVECTION-DIFFUSION-REACTION EQUATION IN TWO-DIMENSIONS: EFFECTS OF NUMERICAL ANTI-DIFFUSION AND DISPERSION-CTFD10
P55-Aerodynamic Performance Study of NACA (653218) Wing with Cuff
P56-Thermochemical Exploration of Supersonic Reacting Flows of a Typical Scramjet Engine Configuration using Open Source CFD Code OpenFOAM-DRDL2
P57-Numerical analysis of fuel mixing physics in gas turbine combustor-cyient
P58-Higher Order Electromagnetics Wave Simulation with PML-DRDL2
P59-A Numerical Investigation to Determine and Compare Drag Characteristics of a Blunt Body with Various configurations of Aerospikes at Mach 6
P61-FLOW CONTROL OVER THE NACA 4415 AIRFOIL USING MICRO CYLINDERS – A COMPUTATIONAL STUDY-SASTRA
P63-Separation dynamics study of a missile launched from helicopter
P65-Verification of 3D Unstructured Grid Based Euler Solver Developed Using Common Framework For NASA CRM Configuration |