VARUN KARTHIK N

adohkq@r.postjobfree.com

733-***-****

CARRER OBJECTIVE:

Being an enthusiastic candidate, having thirst to learn new concepts and develop new skill sets. I do my work sincerely which provide platform to work in your reputed company. ACADEMIC CREDENTIALS:

Bachelor of Engineering P.S.N.A College of Engineering 67.9% May-2020

(Mechanical) and Technology

Higher Secondary School Certificate TVS Matriculation Higher 78% May-2016 Secondary School

Secondary School Leaving Certificate TVS Matriculation Higher 92% May-2014 Secondary School

TECHNICAL SKILLS

SOFTWARE:

Ansys

Solidworks

Abaqus

Revit MEP

Auto CAD

Catia

PERSONAL TRAIT:

Keen observer

Creative and Co-operative

Being honest and loyal

MAIN PROJECT:

FRONT IMPACT TEST USING CARBON FIBRE RE-INFORCED COMPOSITES OBJECTIVE:

Generally cars are quite heavy which is maximum at the front and minimum at the rear. In order to reduce the front weight of the car and to obtain an equal weight balance of the vehicle, the material of the car bonnet is changed to carbon fibre reinforced composites using solidworks and ansys. DESCRIPTION :

In this analysis, four types of CFRP composites are used as a material for car bonnet which also shows less deformation, more strength and stiffness. Compared to stainless steel and aluminium, these materials can be preferred.

As technology is moving towards electrical vehicles which are heavier than the engine cars, CFRP’S can be preferred as a future material for car hoods.

RESEARCH ON AERODYNAMIC EFFICIENCY OF A WING FLAP

OBJECTIVE:

Increasing the aerodynamic efficiency of a wing by adding the feature below the wing flap. This feature tends to increase the lift force and reduces the drag force using ansys software. DESCRIPTION:

In this type of fluent analysis, in order to obtain a higher aerodynamic efficiency the angle of attack angle, inner flap angle, outer flap angle and velocity are changed for each analysis. The values of various analysis are taken and analyzed for each interval using a graph, the set which gives a higher cl/cd ratio yields a better efficiency than others.

This analysis is mainly done to reduce the drag force and to increase the lift force of the wing. BOLTED SATELLITE STRUCTURE ANALYSIS

OBJECTIVE:

It is a material based analysis where the bolt and satellite material is changed for each analysis. Aluminum, Titanium and Kevlar Aramide are the materials used for this analysis. The deformation and equivalent stress of all the three elements are compared for the given acceleration. DESCRIPTION:

In this analysis there are nine cases where in each set the material is changed, that is for one case the bolt material is considered as titanium and the satellite structure is considered as Kevlar aramide same for the other case but vice-versa and also the same material is taken for the structure.

Finally It can be concluded that aluminium (whole structure) shows a lesser deformation than other two elements. In the second case when you take bolt material as titanium and satellite structure as aluminium shows a less deformation. Third case shows considering satellite structure as kevlar aramide fibre and bolt as titanium shows a very less deformation than the above one.

On the whole second case would be recommended assuming bolt material as titanium and satellite structure material as kevlar aramide fibre.

ANALYSIS ON AIRCRAFT FUESLAGE STRUCTURE

OBJECTIVE:

This analysis mainly concentrates on meshing that is how the results are affected by changing the type of meshing, face sizing and edge sizing meshing are done using ansys software. DESCRIPTION:

The material used for the aircraft fuselage structure is aluminium alloy, the aim of this analysis to calculate the deformation, stress, life, safety factor and damage by doing two different types of meshing.

For both face and edge sizing meshing, the structure shows a slight difference in deformation, stress and the safety factor. Edge sizing the structure shows a lesser derfomation, more stress and also minimum value of safety factor varies when compared to face sizing. MINI PROJECT:

DESIGN AND FABRICATION OF MAGNETIC TURBINE

OBJECTIVE:

To meet out the demand for electric power with the help of neodymium magnets, magnetic turbine is designed.

DESCRIPTION:

Magnets produce magnetic fields and can be used in various configurations to generate electricity. The rotating blade can have magnets placed in different locations and can generate electricity in different ways. CERTIFICATE COURSES:

Solidworks, Ansys and Revit MEP certified by CADD centre.

Abaqus CAE certified by Udemy.

INTERNSHIP:

BMW Internship in Goodwin Industries.

Product Development Engineer (CAE Engineer) at Simulation labs.

Design optimization of Multi-plunger positive displacement pump at Mechathon Engineering.

INDUSTRIAL VISITS:

Undergone industrial visit in Roots Industries regarding Stamping, Injection Moulding, die casting, geometric dimensioning and tolerancing.

WORKSHOP:

A two day workshop on Haptics organized by Robokart, IIT Bombay.

One day workshop on IC Engine conducted by Top Engineers. EXTRA CURRICULAR ACTIVITIES:

Member of Quality Circle in school days.

Played Club Cricket

Mime and Debate

PERSONAL PROFILE:

Father’s Name : R.K.Nataraj

Address : Plot No: 22

Kovalan Nagar 7th street,

Madurai -625003.

Date of Birth : 22.10.1998

Languages Known : Tamil, English, French and Hindi (W, R)

Contact this candidate