Mini Project Matric

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BALAJI D

*/***,

Vellalar Street, Katoorani Post Velipattinam

Ramanathapuram District, Tamil Nadu.

Pincode: 623504

Phone No: +91-875*******

************@*****.***

Objective

To establish myself as a successful person with excellence in terms of achievements, creativity and dedication and my skills for the growth of the organization. Areas of Interest

• Aircraft Propulsion.

• Composite Material.

Education

Qualifications

Qualification School/College Board/University Year of Passing

Percentage

Bachelor of

Engineering

(AERO)

Mohamad

Sathak

Engineering

College -

Kilakarai

Anna University

2020

67

HSC

Louis Levail

Matric Higher

Secondary

School

State Board

2016

66.4

SSLC

Louis Levail

Matric Higher

Secondary

School

State Board

2014

73.8

Workshop Details

• Assembling and Dismantle of Quad copterDrones In IIT 2

Date :

Place : Balaji D

Technical Skills

Summary

Computational Fluid Dynamics (CFD), CATIA V5 (Learner) and Ansys (Learner) Project at

Graduation

Title : Design and analysis of Triple mode fuel supply structure for hypersonic engine.

Project brief : This Proposal is a kind of three phase column fuel supply structures for hypersonic aircraft scramjet engine, and three column structures installation of the structure on the base,, such as that existing hypersonic aircraft scramjet engine fuel supply structure can not work long hours, the Sweat cooling of all standing is carried out using fuel while fuel supply. Utilize metallic particles porous media injects fuel into scramjet engine combustion chamber, and it is gentle can to reinforce fuel atomizing Change effect, and promotes the mixing effect of fuel and air. Software used : Solid Work, Ansys

Role : Team leader

Mini Project

Title : Design and Structural Analysis supersonic Fighter aircraft. Project brief : The Purpose of the project is to design a supersonic fighter aircraft. The aircraft will possess a delta wing and tricycle landing gear. Such an aircraft much posses a better maneuver performance and sonic boom doesn’t affect structure and supersonic speed is easily achieved. We have carried out a preliminary weight estimation, powerplan section,weapon loading and aerodynamic parameter selection and analysis with a more in depth study and analysis of aircraft performance and structural characteristics. Software used : Catia V5, Ansys

Role : Developer

Key Strengths • Adaptable, Willing to work in teams.

• Strong analytical skills and inter personal skill Personal Details

Father Name : Dhanasekaran S

Mother Name : Nagarathinam

Date of Birth : 25/10/1997

Known languages : English, Tamil

Hobbies

• Volunteer involvement, Sports, Cooking.

Declaration

I, hereby declare that the information furnished above is correct to the best of my knowledge.

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