Project Engineering

RESUME

PRASANTH.G

No.**,Vivekanandar street, V.P.Singh Nagar,

North Bharathipuram, Puducherry-605009.

Email:********.*********@*****.***

Mob.(India) : 91-888*******

Aspiring for an entry level career in aircraft maintenance/design with a growth oriented

organization of repute.

SUMMARY:

• B.E.Aeronautical engineering from Anna Univesity with exposure to designing tools like

auto cad, catiaV5 and analysis tool namely CFX.

• Strong communication & interpersonal skills with ability to grasp new technical concepts

quickly and apply them effectively.

• Adaptable to any environment and possess skills to work under pressure.

• Possess good leadership skill and time management skill

KNOWLEDGE PURVIEW:

Aerodynamics Propulsion Aircraft structures

AutoCAD,CatiaV5 designing CFD Avionics

EDUCATIONAL QUALIFICATION:

• Bachelor of Aeronautical Engineering in 2013 from GKM College of Engineering and

Technology, affiliated to Anna University, Chennai, First class with CGPA 6.66.

• Diploma in Fire and Safety from National Institute of Fire and Safety, affiliated to

Annamalai University, Chennai in 2013 with First class.

• Higher Secondary from Vailankanni Matriculation Higher Secondary School,

Pondicherry, India in 2009 with 89.95%

• Secondary from Vailankanni Matriculation Higher Secondary School, 2007,with 85.45%

ADDITIONAL QUALIFICATION:

• Autocad, CatiaV5R20, from CADDAM Technologies Private Limited, Chennai 2012,

with ‘A’ Grade.

• Passed in senior grade typewriting examination,2008

PROJECTS:

Title 1: Gas turbine blade cooling using pin fin cooling method(2012-2013)

Description: The project is aimed at the reduction of aircraft gas turbine blade heat using pin fin

cooling setup thereby reducing the damage of turbine vanes. Our study applies a systematic

computational methodology to the leading-edge film-cooling problem. Air is bled from the

compressor, sent directly to channels inside the blades and vanes, and then injected to the

exterior surface through an array of small holes. Film cooling is especially critical at the leading

edge of the turbine blades, since the largest thermal load occurs here and the cooling flow affects

the aerodynamics and heat transfer of the entire airfoil.

Team Size: 4 members

Duration: 6 months

Tools Used: Auto Cad,CatiaV5,CFX

Title 2: Aircraft design project

Description: This project is done for the design of a light medium bomber aircraft with a mach

number at M=0.95 at 11km altitude and having a gross still air range of 4000km. This project

actually aims at the enhancement of the design knowledge.

Team Size: 4 members

Duration: 3 months

Tools used: Auto Cad, Catia

INDUSTRIAL VISITS EXPERIENCE:

• Visited “Airforce station” at Tambaram,Chennai,India

• Visited “National Aerospace Laboratories”(NAL),Bangalore,India and obtained a

knowledge on avionics and navigation systems.

ACCOMPLISHMNETS:

• Participated in NCC camps at Secunderabad and Pallavaram

• Participated in blood donation camp at SRM University,Chennai.

• Served as a co-ordinator and volunteer in various college events.

ACHIEVEMENTS:

• Secured school second in Matriculation examination-2007

• Secured school third in Higher Secondary examination 2009

• Winner of the inter-collegiate basketball tournament.

TECHNICAL SKILLS:

• Catia V5 CADDAM Technologies Pvt. Ltd.

• Autocad As a part of curriculum

• C, C++, MS Office As a part of curriculum

• Typewriting Private

SOFT SKILLS:

• Have a Good Communication skill

• Leadership skill

• Team Worker

• Having good interpersonal skills

PERSONAL DETAILS:

23rd May 1992

Date of Birth :

Gender : Male

Linguistic Ability : Tamil, English, Hindi

(Speak, Read and Write)

Job Location preference : Any location

Contact this candidate