Fresher Resume Format for an Aeronautical Engineer

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RESUME

SUNITA.P

Phone number: +91 9876543210                           D.No:C-16,New Housing Board,

E-mail:sunita028@gmail.com                               CSI Opp,Trichy Road,

Thuraiyur (PO&TK) Trichy(DT),

Tamilnadu,India -621010                                                                  

CAREER OBJECTIVE

                    To pursue a challenging and growth oriented career which would mould me into a complete professional using my technical and interpersonal skills

EDUCATIONAL QUALIFICATION

Name of the Course	Name of the Institution	Board/ University	Year of Passing	Percentage
B.E, (Aeronautical Engineering)	P. B College of Engineering, Sriperumbudur, Chennai	Anna University	2013	70%
Higher secondary School(12th)	SengunthurHr.Sec.School, Thuraiyur	Tamil Nadu State Board	2005	80%
SSLC(10th)	Govt.Boys High School, Sendarappatti.	Tamil Nadu State Board	2003	85%

AREAS OF INTEREST

·        Aircraft Structures

·        Rocket & Jet Propulsion

·        Aerodynamics

·        Computational fluid dynamics

·        Aircraft Maintenance

SOFTWARE SKILLS

·        AUTOCAD

·        CATIA

·        HYPERMESH V.11.Radioss, Optistruct.

·        ANSYS-FLUENT

·        Basic C Programming Language

TRAINING

·        Company Name           :           Fexilon Technologies, Bangalore.

·        Training Duration          :           2 Months

·        Domain                        :           Automobile & Plastic Components/ Aerospace

·        Certification                  :           Master diploma in CAE

About Training           :  TECHZILON TRAINING SOLUTIONS

• Responsible for Mesh generation for  Automotive/Aerospace Anti-Vibrations Components with most restrictive criteria
• Undertaking quality checks according to client’s requirements & correcting on the meshes & prepare them for solution.
• Responsible for Preparing the geometrical clean-up by using Advanced FEM Methodologies.(HYPERMESH V11)
• Accountable for meshing the components as per industrial approach. (2D with or without geometry, 3D meshing, 1D meshing, CFD meshing, refining topology)
• Prepare Analysis set up for various solvers like ANSYS, NASTRAN & ABAQUS
• Creating topology & topographic Design optimization.(Automotive control arm, structural C-clip-bracket, composite air craft structure) 

Meshing Related Projects

FE modeling of door panel of a car using HyperMesh 

• The scope of the project is to build the FE Model with flow-through mesh for crash-analysis of the Door panel of a car.

• IGES Geometry of the cross-member is imported.
• Necessary geometry cleanup done. Identified the features like bolt-holes and slots
• One layer of washer-mesh generated around the holes and cut-outs
• Remaining areas are meshed using linear quad elements.  Less than 5% of trias were used
• Rotating quads are avoided as per requirements. Quality parameters maintained

2D meshing of a car BIW component (Reinf_Asy_Bumper_MTG_LH) using HyperMesh

• The scope of the project is to build the FE Model for stress analysis of Car BIW component.
• Imported the IGES model and cleaned up the geometry.
• Prepared washer-surfaces around holes and cut-outs.
• Identified the features, slots & bolt-holes.
• Generated one-layer of QUAD4 elements around slots & bolt-holes.
• Remaining areas are meshed using linear quad elements.
• Only QUAD4 elements are generated for the entire model.
• Checked for free-edges and duplicates.
• Quality parameters maintained according to client requirements.

3D Hexmesh of a Lower Control Arm of a heavy truck suspension system

• The scope of the project is to build the FE Model for stress analysis of Lower Control Arm of a heavy truck suspension system.
• Imported the IGES model and cleaned up the geometry.
• Used solid mapping for generation of hex mesh within the criteria specified.
• Used QUAD4  elements for ribs.         
• The connection of 3D and 2D elements achieved by inserting one layer of 2D elements into 3D elements of thickness 1/10th of the thickness of the rib.
• Pin was modelled using rigid spider and beam elements

ACADEMIC PROJECTS

Mini Project Title:

DESIGN OF A SUPERSONIC PASSENGER AIRCRAFT

Description:

A Theoretical design of a 150 seaters supersonic passenger aircraft was done with numerical calculations and assumptions. The Main Feature of this fighter is that it can fly at supersonic speed. And we have taken duplov and concord aircrafts as  bases for data collection and we have eliminated the acoustic vibration faced in earlier design of this kind of aircrafts. 

Main Project Title:

DESIGN AND OPTIMISATION OF HYPERSONIC INLET USING CFD ANALYSIS

Description:

In the present study computational tests were carried out to get an understanding of the flow field in a pure mixed compression hypersonic inlet at a free stream Mach number of 6.The design of the inlet for the scramjet stage was undertaken by designing four different inlets and selecting the design with the best performance. The selection criterion was based on the drag generated by the inlet and its susceptibility to boundary layer separation. An inlet that has high compression efficiency produces compressed flow that can do more expansion work and hence produce higher vehicle thrusts as it is expanded over a thrust surface

INDUSTRIAL EXPOSURE

·        Participated in the industrial visit to INS Rajali, Arakonam.

·        Participated in the industrial visit to Albatross Flying Systems, Bengaluru.

CONFERENCES

·        Participated in a conference of experimental aerodynamics by Aeronautical Society of India held at Rajalakshmi Engineering College Chennai.

TRAINING

·        Underwent an In-Plant Training program at Jetwings Technology (Summer 2011), Bengaluru.

·        Participated in a Workshops on MODEL ANALYSIS FOR PERSONNEL ENGAGED IN AEROSPACE, DEFENCE AND MANUFACTURINFING SYSTEMheld at Cambridge institute of technology, Bengalaru (JUNE 2011)

CO-CURRICULAR ACTIVITIES

·        Was a part of Bottle  rocketry event in ASTHRA’1O, a National level Technical Symposium of the Aeronautical Department.

·        Organized the budgetry and managed to conduct ASTHRA’12, a National level Technical Symposium of the Aeronautical Department.

TRAITS

·        Adaptability

·        Diligent

·        Optimistic

PERSONAL DETAILS

·        Father’s Name                         : Mr. TINKU

·        Date of Birth                             : 28.09.1990

·        Gender                                     : Female

·        Languages Known                    : English, Tamil

·        Hobbies                                   : Listening to music, Playing Games

DECLARATION

I Hereby declare that the above furnishdetails are true and correct to the best of my knowledge and I bear the responsibility for the correction of  the above mentioned particulars.

                                                                                                Yours truly,

                                                                         (SUNITA)

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