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Aircraft Project

Location:
Vasant Nagar, Karnataka, India
Posted:
October 23, 2020

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Resume:

KOMALESH B E

S/O ERAPPA B, Balla(V)(P), Mulbagal (T),Kolar(D).

563131

849-***-**** adg8tm@r.postjobfree.com

OBJECTIVE

Seeking a challenging position in your organization and put possible effort to achieve the organisation's goals in turn ensuring growth with in the organisation. I hope to learn new things and aim to maintain a good relationship with the colleagues.

EXPERIENCE

Hindustan aeronautics limited (Engine division) Bangalore 5/07/2019 - 5/08/2019

Student

I have undergone internship in HAL ( Engine division) Bangalore, and I got to know practical knowledge about various engines used in different aircraft's and their work in the duration of one month. EDUCATION

Sri Jagadguru chandrashekaranatha Swamiji institute of technology, chikballapur 2016-2020

Aeronautical engineering

7.68

Sri Vijaya chethana pu college, kolar

2014-2016

Pre-university(class 12th)

88.75

St Anne's high school, Mulbagal

2013-2014

SSLC

89.7

SKILLS

Basic c, c++

MS office word, Excel, powerpoint..

Catia v5, Ansys fluent, Matlab, solid edge, solid works,auto cad.. PROJECTS

Flying wing

An aircraft model which was made by foam material to understand the flight dynamics and design of aircraft. It is basically just the part of the wing which is joined and there is no fuselage which reduces weight of the aircraft and also increases thrust.

Turbojet engine

This is also a model based project which was made to understand the parts of an engine like compressor, combustion chamber, turbine, nozzle. It is basically made to run on fuel(kerosene). We can find the compression ratio of compressor. The thrust produced for a fuel consumption.(still in progress) Effect of sweep on blended wing body aircraft (BWB) This is a software based project and we have used two softwares that is CATIA V5 for designing a model of BWB and ANSYS FLUENT for analysing a BWB model. In this project we have built a model of BWB at different sweep angles from -40 to 55 degree and done analysis on these models and we found the best sweep angle among all these sweep designs. And from the best sweep angle we found the stalling angle of that sweep angle.The duration of this project is almost one year. LANGUAGE

English- read,write,speak

Kannada-read,write,speak

Hindi-read, write

Telegu-read,speak

ACHIEVEMENTS & AWARDS

Completed nptel online courses 1) advanced aircraft maintenance 2) Design of fixed wing unmanned aerial vehicle.

Attended workshop conducted by Happy landing india where we learnt to do the RC model Completed CATIA software.

Participated in online seminar of trends of millennium in arospace to present our project paper in acharya college.

ACTIVITIES

Growing trees to protect nature

Watching sports channel, news...

PERSONAL DETAILS

Date of birth: 25/09/1997

Nationality:Indian

Gender: Male

Address:s/o ERAPPA B, Balla(V)(P), Mulbagal (T), Kolar(D), 563131 PUBLICATION

Effect of stall on blended wing body aircraft.

We published our project paper in IJLTET.

DECLARATION

I hear by declare that the information above is true to the best of my knowledge, I do here by declare that the above particular information and facts stated are true correct and complete to the best of my knowledge and belief.

Place:Mulbagal. Signature

Komalesh B E



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