Aircraft Project

G. Naga Sai Babu

Email Id: ***********************@*****.***

Mobile No: +91-739*******

Career Objective

To enhance my educational and professional skills in a stable and dynamic work place Education Qualification

• Sarada high school

Class 10

8.8

2014

• Sri Chaitanya junior college

Class 12

8.76

2016

• Hindustan institute of technology and science

BTech/Aeronautical engineering

7.7

2020

Academic Projects: (Main Project)

Project Name : Experimental and Numerical analysis on Mechanical properties of carbon-phenolic composites

Team Size & Role : 4 & Team member

Duration : 6 Months

Description:

We prepared the composite with carbon fiber and phenolic resin. The tensile properties of C – Ph composite has been obtained form the tensile test that was done onthe specimens in the MTS Landmark Fatigue Testing Machine.The Numerical results of the tensile, fatigue and flexural tests are obtained by the computational analysisof our Carbon – Ph material, which is done by giving the tensile properties of the material as the inputsin the software.From the results, we came to a conclusion that the numerical tensile test result which is the maximumload experienced by the model

Contribution:

As a team member, I taken the responsibility of the whole project that have to complete in given time. As I did the good coordination with the teammates to gather the full information about the project and the testing and analysis of whole project was done with the help of our gide. Academic Projects: (Mini Project)

Project Name : Design of 6-Seater business jet Aircraft Team Size : 2

Duration : 12 Months (6th and 7th semesters)

Description:

In the first six months, we have calculated weight estimation, powerplant selection, airfoil selection and wing design parameters, done the performance analysis of the aircraft during landing and take-off. In the next six months, by taking the values obtained in the first set as input, the load factors during various phases of flight is calculated and the V-n maneuver diagram is drawn. The load distribution of wing in using schrenk’s curve method was found which is very sufficient for the design requirements. We used pratt and whitney canada Pw 545c Enginehaving trust of 3952lbs and take off weight 6123 kg.Hence Aircraft has been designed with various performance and aerodynamic parameters calculation, which can carry upto 6 members with all the facilities inside.

Software and Technical Skills:

AUTOCAD (basic)

Solidworks (basic)

Ms office

Personal Traits:

Good communication skills

Team oriented

Quick learner & Interested in learning new things.

Positive thinking & Hard worker.

Being self-motive.

Co-Curricular Activities:

Industrial visit to Sathish Dhawan Space Centre-ISRO, Sriharikota.

Achived 8th position in MYVI competition.

Workshop on “ Advances in Aircraft Structural Design” in HITS Chennai.

Internship Program in AIR INDIA Hyderabad basic structural parts & NDT inspection, Basic level maintenance.

Extra Curricular Activities:

Vice-president for Rotaract club of Hindustan university for year 2019-2020.

I was made incharge of polio camp conducted in near by village.

One of the Student coordinator for NSS cell.

One of the student coordinator for aeronautical department. Personal Profile:

Name : G. Naga Sai Babu

Father's Name : G. Nageswara rao

Date of Birth : 01-JAN-1999

Gender .: Male

Marital Status : Single

Nationality : Indian

Languages Known : English, Telugu & Tamil

Permanent Address : 1-110, Devarapalli village, parchur mandal, prakasam district, A P -523169

Declaration:

I hereby declare that the above written particulars are true the best of my knowledge and belief. Date : 06/07/202

Place : Devarapalli G. Naga Sai Babu

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