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Aeronautical Engineer Matric

Location:
Chennai, Tamil Nadu, India
Salary:
2.9lpa
Posted:
August 09, 2021

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Resume:

Mohan Kumar. B

Aeronautical Engineer

A passionate engineer seeking for a job in challenging and healthy work environment demanding all my skill and effort to explore

mohankumar721152@gmail.

com

638-***-****

chennai, India

linkedin.com/in/mohan-

kumar-b-517a4b201

github.com/mohan1998

TECHNICAL AND

SOFT SKILL

CATIA ANSYS

Microsoft office

Excel Python

Perseverance

Team work

Efficiency

leadership

LANGUAGES

Tamil

Native or Bilingual Proficiency

English

Full Professional Proficiency

AREA OF

INTERESTS

Designing and

propulsion

Programming

Analysis structural

designing

EDUCATION

B.E in Aeronautical Engineering

Jeppiaar Engineering college

2016 - 2020, 6.87 CGPA

Higher Secondary School (HSC)

Peniel Matric Higher Secondary School

2015 - 2016, 68.5 %

Secondary School (SSLC)

Peniel Matric Higher Secondary School

2013 - 2014, 76.5%

CERTIFICATES

CATIA (2019)

designing software

Participation certificate ( 09-06-2020 )

Webinar on career "opportunities for Aeronautical Engineering" conducted by MLR Institute of Technology, Hyderbad

Certificate of participation ( 11-06-2020 )

Attended webinar on " INNOVATION IN JET CONTROLS" by Jeppiaar Engineering College, Chennai ICONSTEM-2020 6 International conference on science, Technology, Engineering and Management (15-07-2020 )

It is conference meet where every publish there journal and project papers . Conducted by Jeppiar Engineering College, Chennai.

Digital Marketing

It is course conducted by GOOGLE

PERSONAL PROJECTS

CFD ANALYSIS AND FLOW STIMULATION OVER RE -ENTRY VEHICLES IN DIFFERENT PLANETS (2019 - 2020)

Designed heat shields of different Dimensions to study the effect of nose radius on the aerodynamic properties

Modelled the simulation environment and analysed the flow properties in different atmosphere conditions

DESIGN MODIFICATION OF SUKHOI-SU57 COMBAT AIRCRAFT (2018 - 2019) Reducing weight of the aircraft by 45% to achieve high maneuvering speed and higher fuel efficiency in combat condition

Modification of the airfoil design to allow high lift and reduce drag ratio to achieve high Mach no INTENSHIP

Aerospace Technical publication and engineering services (06/2021 - 07/2021) Aerotic Technology, Bangalore



Contact this candidate