Karan Dholkaria
*/***, ********* ***, ******* nagar 5, Chembur-E, Mumbai, Maharashtra, ***************@*****.***,
https://www.linkedin.com/in/karan-dholkaria-7a1216195/
INDUSTRIAL EXPERIENCE
Simulation Lab, Pune – CAE Engineering Intern
January – April 2020
Worked closely with design development and testing team members to design and develop robust solutions meet client requirements for functionality, scalability and performance.
HAL, Aerospace Division, Bangalore — Intern
June 2018 - July 2018
●Delivered expert clerical support by efficiently handling wide range of routine and special requirements.
RESEARCH WORK
“Combustion Characteristic of an Array of Energized Candle Flame”, published in the Journal of Material Science and Mechanical Engineering (JMSME), with the conference held in October 2017, at Jawaharlal Nehru University, New Delhi.
Attended SWAYAM 2018 (Symposium and Workshop for Analytical Youth on Applied Mechanics), held at BITS Goa, in July 2018, and presented an extension of our aforementioned work.
“A Spatial Perspective on Metallized Combustion Aspect of Rockets”, selected for presentation at the IEEE Aerospace Conference, held in Big Sky, Montana from March 2 to March 9, 2019.
ADDITIONAL INFORMATION
GRE Test score: Verbal reasoning- 146/170, Quantitative reasoning- 168/170, Analytical writing- 2.5/6.
IELTS score: Listening-8, Reading-7, Writing- 6, Speaking- 7.5 and Overall band score- 7.
SKILLS
Team Management
Communication
Stress Management
Teaching
Negotiation
SOFTWARE AND PROGRAMMING LANGUAGE
MS Office
CATIA
ANSYS
Solidworks
AutoCAD
Unigraphics Nx
C & C++
EDUCATION
LANGUAGES
English, Hindi, Marwari, Marathi, Basic German
Degree
Institute
University
Percentage
Year
B. Tech.
Aerospace cEngineering
SRM Institute of Science and Technology
SRM University
76.71%
2019
H.S.C.
Chandrabhan Sharma College of Arts, Science & Commerce
Maharashtra State Board
76.77%
2014
S.S.C.
General Education Academy
Maharashtra State Board
81.33%
2012
PROJECTS
Stratified flickering behavior of candles in array of diffusion flame.
Shock Induced Boundary Layer Control using Ram air Pressure.
Investigation on flame stabilization of Bluff Body: Blockage Effect.
Spatial Perspective on the Metallized Combustion Aspect of Rocket.
I confirm that, the above information is true and correct to the best of my knowledge.
Date Sign
Karan
Dholkaria