Engineering Assistant

JEEVITHA S

E-mail id: ***********************@*****.***

Contact: 890-***-****

OBJECTIVE:

To show my Innovation and Creativity throughout my career and to learn each and every day to emerge as an Eminent Professional

ACADEMIC EXCELLENCE:

Specifications Institutions Year Of

Passing

Percentage

M.E (Aeronautical)

(PT)

Madras Institute of

Technology, Chennai

2016 8.23

B.E (Aeronautical) Hindusthan College of

Engineering and Technology,

Coimbatore

2012 89

+2 S.N.G. Girls’ Higher

Secondary School,

Thiruthangal.

2008 86.5

10 S.N.G. Girls’ Higher

Secondary School,

Thiruthangal.

2006 90.6

TECHNICAL SKILLS:

SOFTWARE KNOWN: AutoCAD, CATIA, ANSYS, GAMBIT

AREA OF INTEREST:

● Flight Dynamics

● Propulsion

● Structures

STRENGTH:

● Good Initiator

● Committed to work

● Planning and executing the task

PAPER PRESENTATIONS:

● “Air Crash Analysis in Helicopters” in Jaya Engineering College, Chennai andHindusthan College of Engineering and Technology, Coimbatore

● “Implementation of Nano materials in Aerospace Industries” in Excel College of Engineering, Salem

● “High Temperature Materials” in Nehru College of Engineering and Technology, Coimbatore.

ACHIEVEMENTS:

● University Rank Holder (39th rank) in my Bachelor Degree

● Secured a score of 28.6 in GATE 2013

● Class Topper during my Schoolings

PROJECT:

M.E. PROJECT:

ORGANIZATION: MADRAS INSTITUE OF TECHNOLOGY, Chennai PROJECT TITLE: ACOUSTIC CHARACTERIZATION OF CO-FLOW JETS UNDER DIFFERENT VELOCITY RATIOS

PROJECT GUIDE: Dr. S. THANIGAIARASU, Assistant Professor, MIT, CHENNAI DESCRIPTION:

The jet noise produced by the single jet is proved to be reduced by introducing Co-axial jet.The velocity of the primary jet is kept at Mach 2 and by varying the secondary jet as 0.5, 0.6and 0.7, the analysis is done using GAMBIT and ANSYS B.E PROJECT:

ORGANIZATION: HINDUSTHAN COLLEGE OF ENGINEERING AND TECHNOLOGY

PROJECT TITLE: AIR CRASH ANALYSIS IN HELICOPTERS

PROJECT GUIDE: Mr. S. PRADEEP JOHNSON, Assistant Professor, HCET, Coimbatore.

DESCRIPTION:

The analysis was carried out for ground crash in Helicopters using Hyper mesh and LS Dyna.“DEPLOYABLE ENERGY ABSORBER” is employed to absorb the energy released on impact on the surfacedue to crash. PERSONAL DETAILS:

Husband’s Name : MR. S.Radhakrishnan

DOB : 23/12/1990

Age : 28

Sex : Female

Marital Status : Mar

Bharathipuram, Chromepet, Chennai-44.

Experience : 3.3 years

Nationality : Indian

Languages known : Tamil. English, Hindi

Hobbies : Listening Music and Reading Books

DECLARATION:

I hereby declare that all the details and particulars furnished above are true to the best of my Knowledge.

REFERENCES:

Mr. S. Thanigaiarasu : 944-***-****

(AP, Department of Aeronautical Engineering, MIT, Chennai.) Mr. K. Bijil Kumar : 967-***-****

(Project Manager, Pricol Technologies, Coimbatore)

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