Aeronautical Engineer

MAHARSHI VYAS

+91-846*******, +91-799******* adl07d@r.postjobfree.com Vadodara, Gujrat, India

EDUCATION

Bachelor of Technology in Aeronautical

Engineering

Parul University

LANGUAGES

GUJRATI

Native

Hindi

07/2018 - Ongoing LIMBDI, VADODARA,

GUJRAT

Native

Diploma in Aeronautical

Engineering

Gujrat Technical University

CGPA

9.7 / 10

English

Proficient

06/2015 - 04/2018 AHEMDABAD, GUJRAT SKILLS

PROJECTS

Design and Modelling of RC Plane with Cargo

Dropping Door Mechanism

SINGING

ADVANCE BASIC COMPUTER COURSE

HTML AUTOCAD

2017 - 2018 Location

We did our project in the last year of diploma at Parul University. In this project, we built an RC aircraft, capable of dropping any small object from the air. It was also able to fly longer and lift more weight. Due to this project, we learned calculation of its strength and its aerodynamic shape, apart from that we also learned about its design, and we learned how its engine works and how it is appointed. Design and Analysis of Airfoil

AEROMODELLING

ACHIEVEMENTS

PUBLISHING A RESERCH PAPER ON

OUR PROJECT IN IJIRSET

2018 - 11/2019 PARUL UNIVERSITY

This project is aimed to obtain the velocity and pressure profile, Production of Lift and Drag by Airfoil at particular AOA, separation of flow over an Airfoil, the graph of variation in coefficient of lift with AOA

(cl-α) and coefficient of Drag with AOA (cd-α) is plotted by using the Ansys Software for an NACA 4412 and NACA 0018 Airfoil. We use fluent module in Ansys for Analysis. CFD plays an important role in design and optimization process. In this project, we are comparing the Computational result with the standard result.

DISTINCTION AND FIRST CLASS IN

CLASSICAL SINGING EXAM

DISTINCTION IN ENTERENCE EXAM AND

FIRST CLASS IN 1ST YEAR IN BRUHAD

GUJRAT SANGEET SAMITI (GANDHRVA

UNIVERSITY)

Coefficient of lift for Asymmetric airfoil is higher than a symmetric Airfoil for

Same AOA and same chord length. Stalling angle for an Asymmetric airfoil is lower than a symmetric airfoil for a same AOA and chord length. Drag force in Asymmetric airfoil is significantly higher than symmetric airfoil. The maximum coefficient of lift for symmetric airfoil is 1.622 and stalling angle is20. The maximum coefficient of lift for Asymmetric airfoil is 1.93, which will get at 20 AOA, stalling angle is 20, above the maximum lift coefficient the high wake region is produce above the surface of an airfoil nearer to its trailing edge.

2 TIMES RUNNER UP OF TECH

EXPO EVENT IN PARUL

UNIVERSITY

ATTAINED COMBINED ANNUAL

TRAINING CAMP OF NATIONAL

CADET CORPS AND FLYING CAMP

IN NATIONAL CADET CORPS

PROJECTS

Modifying Fuselage Seating Arrangement Of

Learjet 45 Aircraft

2019 - Ongoing PARUL UNIVERSITY

The aim of thi project is to “MODIFYING FUSELAGE SEATING ARRANGEMENT OF LEARJET 45 AIRCRAFT”. Business jet or private STRENGTHS

QUICK LEARNER AND

ABILITY TO WORK UNDER

PRESSURE

Jet is a term describing a jet aircraft, usually of smaller size, designed For transporting group of people or wealthy individuals. The project Involves design of fuselage of Learjet 45 such that it can accommodate 10 persons at full seating layout. It is design is such way that is can be helpful during medical emergency also. It is made in such way that the seat can be converted to stretcher. Moreover, it will provide the level of comfort that a business jet is expected to provide.

We understand how to use same space to

Create more capacity of passengers and also how we convert seats to a stretcher. We come up with the so much of different ideas and at last, we finalized this idea. We understand the calculation to arrange the fuselage seating and arrangement of emergency exit. By this research, we now knew that which types of materials used in business jet aircraft and which materials we need in our aircraft.

• By the calculation, we can understand how much materials we have to take.

NIMBLE-WITTED

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