SATHYA PRIYA J

EMAIL: ac86zt@r.postjobfree.com MOBILE: +91-950*******

CAREER OBJECTIVE:

As a CAE Engineer and Analyst working with Thermal and Aero model build and simulation - CFD in automotive industry for the past 2.10 years endeavoring a zestful position for aspiring to contribute to the growth of the organization. CAREER SUMMARY:

COMPANY NAME : FORD TECHNOLOGY SERVICES, INDIA

(Deputed by: Satyam Ventures Engineering Services Pvt Ltd) DESIGNATION : CAE ENGINEER / ANALYST

DURATION : From July 2016 to till date

EDUCATIONAL QUALIFICATION:

• B.E - Aeronautical Engineering at K.C.G College of Technology, Chennai; CGPA: 8.46 – Anna University 28th Rank, 2012-2016 Batch

• HSC at S.H.N Ethel Harvey Girls Higher Secondary School, Sattur; Aggregate: 91.42%, Completed in March 2012

• SSLC at Dr. Radhakrishnan Vidhyalaya Matriculation Higher Secondary School, Sattur; Aggregate: 88.8%, Completed in March 2010 PROFESSIONAL EXPERIENCE:

Currently working in Ford Technology Services, India as Team Lead of team size – 03 PROJECT 1: Full Vehicle CAE – CFD model build for Cooling (Engine & Exhaust)

&Thermal simulation (Support –FNA, FOE & FOA)

RESPONSIBILITIES:

• Understanding the requirements from the client side, preparing query and clarifying document

• Geometry cleanup and surface meshing by capturing all important components without compromising the quality parameters

• Model build is done in order to reduce the heat flow across all the thermal parts based on the CFD concepts

• Underhood parts are modeled in detail for Taitherm (RadTherm) and Fluent TOOLS USED:

Teamcenter, Vis-Mockup & ANSA

ACHIEVEMENTS:

Certificate of Excellence is given for executing projects in CAE - CFD (Cooling and Thermal)

PROJECT 2: Full Vehicle model build for Aero Acoustics – Aerodynamic shape study and Interior Cabin Noise Study – CAE (CFD-Aero for FNA) RESPONSIBILITIES:

• Understanding the requirements from the client side, preparing query and clarifying document

• Aerodynamic geometry cleanup and surface meshing (STL mesh) is carried out on both surface model and in FE model meshing is done

• Aerodynamic shape study and Internal Cabin Noise study model build is done as per client requirement

• A surface parts are studied in detail and Quality parameters are maintained as per client needs

ACHIEVEMENTS:

• Model build (Taping study) is done with the high quality checks which results in reduction of drag by improving the efficiency of the vehicle

• Recognized by the clients for the improvisation of quality in the model TOOLS USED:

Teamcenter, Vis-Mockup & ANSA

PROJECT 3: Material Data Collection and Validation for CAE-CFD model

(Support – FNA, FOE & FOA)

RESPONSIBILITIES:

• Material data collection is done for cost and time reduction for all the components of a vehicle to reduce the erroneous information thus in improving the efficiency Material data is collected for all the components of the vehicle from Bill of Materials (BOM) from the CAD drawing sheets

• Components are exported to CATIA for the validation process

• Material confirmation is done by the test results received from the supplier and D&R Engineer and is recorded in Ford Material Database

• Boundary condition setup in done TaiTherm (RadTherm) for CFD analysis TOOL USED:

Teamcenter, Teamcenter Lifecycle Vismockup, CATIA V5, TaiTherm

(Radtherm), MS-Excel

ACHIEVEMENTS:

• Appreciation received from the clients of all regions for developing a successful process flow for all the milestone of a vehicle

• Reducing the time in obtaining the material information by formulating a new process flow

• Analysis reports approximately matches with the test data results PROJECT WORK DURING GRADUATE PROGRAM:

Design of Propeller Driven Trainer Aircraft-Aerodynamic Analysis and structural analysis - The weight of the propeller driven trainer aircraft is reduced by placing the loads on different positions which in turn increases the fuel efficiency of the aircraft.

Upgradation of free jet into a miniature supersonic wind tunnel – Computational and Numerical simulation - Experiments and computational methods are used to investigate the flow properties. Mach 2.5 convergent divergent nozzle is designed using method of characteristics. Flow properties for that nozzle are analyzed in computational method and the nozzle obtained is fitted in free jet facility. The free jet facility can be used as a miniature supersonic wind tunnel. SKILLS KNOWN:

• Experience in ANSA and Teamcenter

• Basic knowledge of CATIA, Auto CAD, MSC Nastran and C language

• Knowledge of Automotive systems and its components

• Basic knowledge in vehicle manufacturing

• MS-Office

PERSONAL DETAILS:

Date of Birth : 16th November 1994.

Father’s Name : Mr. R. Janakaran

Address : BS1, Kanna Enclave, Sahadevan street,

Santhosapuram, Medavakkam, Chennai

- 600100.

Marital Status : Married

Languages Known : English (W/R/S), Tamil (W/R/S), Hindi (W/R) & Telugu (S) Hobbies : Drawing, Playing throw ball & Travelling. ACKNOWLEDGEMENT:

I reaffirm that the above furnished details are true to best of my knowledge.

(SATHYA PRIYA J)

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