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TECHNOLOGY TRAINING & RESEARCH CENTER (TTRC)

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Saturday, 08 June 2013 12:06

TTRC Department of Materials Engineering and Finite Element Analysis

1. Finite Element Analysis and Simulation Orthogonal Cutting Process.

Associate: Sreejith N, M-Tech, Cochin University of Science and Technology.

  • Explicit Dynamic Analysis is carried out to observe the stress distribution on Cutting tool, Pre-processing, solving and post processing doneusing ANSYS-LSDYNA.

2. Soil - Structure Interaction Studies Of Offshore Wind Farm Structure with Conventional And Reinforced Soil Foundation Using FEA Methods

Associate: Miss.Anooja Joseph, M.Tech Cochin University of Science and Technology

  • Intend to study the response of the conventional offshore foundation using ANSYS FEA, to predict the enhancement in the strength ofthe foundation with reinforced soils.and to analyse the dynamic response of the structure by consecutive waves hitting the structure.

3. Finite Element Analysis of Folded Plates to observe the comparative study on Classical Method and Numerical Method.

Associate: Tibu Chacko, M-Tech, MA College of Engineering.

  • Static structural Analysis is done to observe the mid span deflection, force distribution on the folded plate structure.Pre-processing, solving and Post-processing done using ANSYS APDL.

4. Static Structural Analysis of Steel Fibre Reinforced Concrete Deep Beam with and without Opening.

Associate: Nerin.K.Antony, M-Tech, MA College of Engineering.

  • Static Structural Analysis is carried out to observe the mid-span deflection with varying distance between the load span areas. The Pre-processing, solving and Post-processing is done using ANSYS APDL.

5. Finite Element Analysis and Modelling of Flat slab and Grid Slab Structure.

Associate: Muhammed Yoosaf K T, M-Tech, MA College of Engineering.

  • Static Structural Analysis is carried out to observe the deflection in the mid-section area of the Flat slab and Grid slab structure, loads distribution in the critical region of both slabs.Pre-processing

6. Finite Element Analysis and Modelling of RC Beam Strengthened with FRP Laminates.

Associate: Martina Paulose, M-Tech, Cochin University of Science and Technology.

  • Transient Structural Analysis is carried out to observe the deformation of the reinforced structure, reinforced structure with FRP laminates .Pre-processing, solving and post-processing is done by using ANSYS APDL.

7. Finite Element Analysis and Modelling of Cylindrical Shell Structure.

Associate: Ashique Jose, M-Tech, MA College of Engineering.

  • Static Structural Analysis is carried out for the cylindrical shell structure to observe the pressure distribution over the surfaces .Pre-processing, solving and post-processing is done using ANSYS APDL.

8. Finite Element Analysis to observe a performance –based approach for evaluating fire resistance of Pre-Stressed concrete double T-beam.

Associate: Rohini G Nair, M-Tech, Cochin University of Science and Technology.

  • Transient Thermal Analysis, Transient Structural Analysis and coupled analysis is carried to observe the thermal effect on the strand (pre-stressed reinforced).Pre-processing, solving and post-processing is done using ANSYS APDL.

9. Finite Element Analysis observes Axial and Flexural Performance of Square RC Columns   Wrapped with CFRP under Eccentric                 Loading.

Associate: Safna M S, M-Tech, Cochin University of Science and Technology.

  • Linear and Non-linear Static Structural Analysis is carried to observe compression pressure distribution on the surfaces of the square RC Column structure wrapped with CFRP .Pre-processing ,solving and post-processing is done using ANSYS APDL.

10. Finite Element Analysis and Modelling is carried to observe the effect of cooling fluid in the Engine Cavitation considering Piston- Cylinder Assembly forces.

Associates: Basil George, Paulcy Issac, Gokul P R, Jojo Thomas, Josy Jose, B-Tech (Mech), Ilahia College of Engineering.

  • Static, Acoustic (Fluid Coupled), Thermal and Harmonic Analysis is carried out to observe the effect of cooling and pressure distribution in the  engine cavitation considering Piston-Cylinder Assembly.

11. Finite Element Analysis is carried out to observe the study of Biomimetic Applied for Design Optimization of Cylindrical Shell Structure.

Associate: Remya P M, M-Tech, Cochin University of Science and Technology.

  • Static Structural Analysis Macro has been written using ANSYS log file, Design Optimization has been done to get coordinate of shell  structure. Pre-processing, solving and post-processing is done using ANSYS APDL.

12. Finite Element Analysis of Flange Joint.

Associates: Bivin Thomas, Jabin M, Benjamin, Jerin Jose, Jerome J P, B-Tech, Amal Jyoti College of Engineering.

  • Static Structural Analysis is carried out to observe the deformation and stress occurs due to pressure distribution in flange joint .Pre-  processing, solving and post-processing is done using ANSYS WORKBENCH.

13. Finite Element Analysis is carried out to observe The Seismic Analysis –Earth quake effect on the storage tank.

Associates: Parvathy Krishnakumar, Anumodh A.S, Shaharban Shaful, Ejas P J, M-Tech, Cochin University of Science and Technology.

  • Modal, Transient Analysis is carried out to observe the earth quake effect on the storage tank at bottom section .Pre-processing, Solving and  Post-processing is done using ANSYS APDL.

14. Finite Element Analysis of Aircraft Wing Structure and Design Validation.

Associates: Blesson Raju, Nadheer A, Anujith M, Alexander Achankunju, B-Tech (Aero) Mount Zion College of Engineering.

  • Static Structural Analysis of Trainer Aircraft Wing Structure is carried out to validate the Design Structure .Hand calculation; Modelling is done  using CATIA, Pre-processing, solving and post-processing is done using ANSYS WORKBENCH.

15. Finite Element Analysis of Aircraft with GPS & INS/ILS Technology.

Associates: Jacky Joseph, Abdul Majeed, Tito Antony, Vibi John,Ajay Shankar, B-Tech (Aero), Jawaharlal College of Engineering.

  • Fabrication, Modelling and installation of GPS, INS/ILS Technology is done, Static structural Analysis of Engine Mount is carried to validate the  design structure of the aircraft. Modelling is done using CATIA, Pre-processing, solving and Post-processing is done using ANSYS WORKBENCH.

16. Finite Element Analysis and Modelling of 5 Seater Short Range Passenger Aircraft.

Associates: Arshath Ayoob, Arya Sanil, Vishnu S Nair, B-Tech (Aero), Mount Zion College of Engineering.

  • Hand calculation of Aircraft Design parameters, Modelling and Static Structural Analysis of Fuselage and Wing Structure assembly is carried out  to validate the Design structure of the Aircraft.Pre-processing , solving and  post-processing is done using ANSYS WORKBENCH.

17. Finite Element Analysis, Modelling and Design Optimization of Snake Boat.

Associate: Devdas P, M-Tech, Cochin University of Science and Technology.

  • Modelling of Snake boat Structure is done using CATIA, Static and Modal analysis is carried out to validate and optimized the design structure  of the Snake Boat.Pre-processing, solving and post-processing is done using ANSYS WORKBENCH.

18. Finite Element Analysis and Modelling of Micro turbine Compressor.

Associate: Manikandan H, M-TECH, KMEA College of Engineering.

  • Modelling is done using CATIA, Static and Modal Analysis is carried out using three different materials to observe the structure deformation  and stress distribution while rotating at different Velocities. Pre-processing, solving and post-processing are done using ANSYS WORKBENCH.

19. Finite Element Analysis, Modelling and Design Optimization Billet Size for minimum Forging Load.

Associate: Arun KS, M-Tech, St. Joseph College-PALA

  • Static Structural Analysis followed by the design optimization is carried out to obtain the minimum forging load for Billet Size.Pre-processing,  solving and post- processing is done using ANSYS APDL.

20. Numerical Investigation On Optimum Layout Of Submarine Pipe Laying

Associate: Arun Kumar K K, M Tech, Cochin University of Science and Technology

  • To establish a scheme of numerical simulation to determine the hydrodynamic properties for various layouts of submarine pipes and to suggest  an optimum layout for minimum hydrodynamic forces.

21. Finite Element Analysis of RF MEMS Switch.

Associates: Minni J Kappen, Therasa Tomy, B-Tech-Electrical, Rajagiri College of Engineering.

  • Thermal-structural coupled analysis is carried out to observe the deformation in the mid span section of RF MEMS Switch.Pre-processing,  solving and post-processing is done using ANSYS APDL.

22. Finite Element Analysis of Ceiling Fan Shank Structure.

Associates: Agin Jose, Geo Antony, Krishnadas, Cherian, B-Tech, Amal Jyothi College of Engineering.

  • Static Structural analysis is carried out to observe the deformation and pressure distribution over the ceiling fan shank structure.Pre-  processing, solving and post-processing is done using ANSYS WORKBENCH.

23. Finite Element Analysis is carried out to observe the flexural behaviour of Reinforced and Pre-stressed Concrete Beams.

Associate: Zaroof Mohammed, M-Tech, NITK, Surathkal.

  • Static Structural is carried out to observe the crack initiation and failure of whole structure at 16000 lbs.Pre-processing, solving and post-  processing is done using ANSYS APDL.

24. Finite Element Analysis and Modelling of Aircraft Searcher Mak-ll (UAV)

Associate: Lt. Nitin Manocha, M.tech, CUSAT.

  • Hand calculation of Searcher Mak-ll UAV ,Modelling is done using CATIA Static structural Analysis is carried out to valid the design structure of  UAV. Pre-processing,solving and post-processing is done using ANSYS WORKBENCH/APDL.

25. Analysis of Crack growth in Rubber

Associate: Shiva Prasada B, Santhosh K.R, Sriharsha.R, B.E

  • A fracture analysis, combination of stress analysis and fracture mechanics to observe the crack initiation and propagation in the Rubber.

26. Finite element analysis of pressure vessel manifold

Associate: Umesh Naik.R, Kishan Kumar Rai, B.E

  • A Thermal and Structural analysis of the pressure vessel manifold using finite element method to determine the structural and thermal  properties of the pressure vessel manifold and to determine the safe limits.

27. Thermal & Structural analysis of Pressure vessels

Associate: Simon Mathews, Nibu Sam Chacko, Vikas Bangera B.E

  • Thermal-Structural coupled field analysis of pressure vessel to get the stress distribution and validate it using ASME Code Section VIII Div 1.

28. Thermal and Structural analysis of heat Exchanger Shell

Associate: Appu C.Kurian, M.Tech,

  • Thermal Analysis of heat exchanger Shell to get the temperature plots and Thermal-Structural coupled field analysis of shell to get the stress   distribution then validate it using ASME Code Section VIII.

TTRC Department of Computational Fluid Dynamics

1. CFD optimization of rear diffuser in a Sedan to minimize drag

Associate:  Kurian Jory, M.Tech CAD/CAM, Vellore Institute of Technology.

  • CFD analysis on sedan class car was done with various under body rear diffuser configuration to understand the variation in flow pattern and drag force. The diffuser dimension was varied in lengthwise and angle wise and drag variation was studied. This data can be used for further optimization of car diffusers.

2. CFD optimization of Heat sink.

Associate:  Jestin K, Abey RajanJustin Sunny, Midhun V.M, Deepak Johny, B.tech mechanical, Ilahia College of Engineering

  • CFD simulation of heat sink was to attain optimal configuration of base plate thickness, fin frequency, and to select efficient base plate material.

3. CFD simulation of cross flow heat exchanger.

Associate:  Shanulraj, Kunjunni M, Sanjay N.S -B.tech Mechanical, Toch -Cochin

  • CFD simulation of cross flow heat exchanger was done to measure the performance and to find out the resulting outlet temperature of hot and cold fluid. The hot fluid was air and the cold fluid was water

4. Pressure distribution study using CFD and stress analysis in FEA on the ceiling fan shank

Associate:  Agin Jose, Geo Antony, Krishnadas, Cherian, B.tech mechanical, Amal Jyothi College of Engineering

  • CFD simulation of ceiling fan was done to find the pressure acting on fan blades to apply the details in stress analysis.

5. Parametric modelling of ram air channel using CFD.

Associate:  Bibin Joseph, Midhun Menon, Jayasanker N, Grace Sarah Gabriel B.tech Aeronautical, Mount Zion College of Engineering

  • Ram air channel of fighter aircraft was parametrically modelled using CFD which can be used for optimization of ram air channel components at minimum drag and pressure loss.

6. Wing structure analysis of searcher mark-II UAV

Associate:  Lt. Nitin Manocha,Naval Institute Aeronautical Technology M.Tech, CUSAT

  • CFD simulation wing was done at different angle of attack to find the pressure force action on the wing and the variation of drag and lift forces. This result was used to do the structural analysis.

7. Nose cone design

Associate: Heigurujam Don Singh,

  • For different nose cone model the fluid flow is studied and it is observed in which model the shock wave is mild and velocity profile is uniform.

8. Pressure recovery optimization of Centrifugal Compressor using Advanced CFD tools

Associate: Pothuri. Venkateshwara Rao

  • The pressure recovery of the centrifugal compressor studied, by varying the angle of the diffuser and the most suitable angle for the desired outcome was studied.

9. Gas Turbine silencer (industrial) design optimization

Associate: Shahid Nadeem, M.Tech

  • Avoiding the turbulence created inside the silencer to reduce the vibration and failure, by guiding the flow.

10. Design of different inlets for fully developed flow in axial duct fan

Associate: MD. Aslam

  • Different types of inlet with varied properties are designed for the fully developed flow in the axial duct fan

11. Fluid flow analysis of piezoelectric  valve less micro pump

Associate: Mohan Das A N, B.E

  • A Study on the Fluid flow analysis was done for the piezoelectric valve les micro pump was done to evaluate the best possible mode.

12. Anti-icing system of aircraft wing

Associate: Jagannath Reddy, M.tech

  • Analysis of heat transfer from piccolo tubes to the wing surface, which maintains a temperature on the surface to prevent icing.

13. Estimation of aerodynamic characteristics aircraft using CFD Simulation

Associate: M.D.Zameer, M.tech

  • Simulation carried out in fluent for a fuselage to find out lift and drag values at various angle of attack.

14. Drag prediction around aircraft wing

Associate: Som Dutt.M.Patil, M.Tech.

  • Simulation carried out in fluent for a aero foil (2d) & wing (3d) to find out lift and drag values at various angle of attack.

15. Analysis of flow performance through annular curved diffusing duct using CFD

Associate: Ashok.M, M.Tech

  • Simulation of fluid flow inside the annular curved diffuser duct without hub, with hub and with hub of varying cross section and finding the pressure recovery and pressure loss.
Last Updated on Saturday, 13 September 2014 08:02
 

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