Aeronautical engineering

NIKITHA GUDISE

Mobile: 903*******

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

SUMMARY

•I intend to be a part of an organization where i can constantly learn and develop my techincal and management skills and make best use of it for the growth of the Organization.I look forward to establishing myself by adapting new technologies as well.

EDUCATION

Bachelor of Technology in Aeronautical Engineering 2016-2020

MALLA REDDY COLLEGE OF ENGINEERING & TECHNOLOGY,Hyd, India CGPA- 7.8

Board of Intermediate Education(Maths,Physics,Chemistry) 2013-2015 SRI CHAITANYA JUNIOR COLLEGE,Hyd, India GPA- 8.8

Board of Secondary School Education(SSC)

VIDYA BHARATHI HIGH SCHOOL,Hyd, India GPA- 8.3

TECHNICAL SKILLS

Programming

Operating systems

Designing Tools

: C, C++.

: Microsoft word, MS Office.

: AUTO CAD, CATIA, ANSYS, MATLAB.

ACADEMIC PROJECTS:

PROJECT: Fluid Flow Analysis of Aerospike Nozzle.

Team Size : 3

Position : Team leader.

Software : Catia, Ansys

Description: An aerospike nozzle is the truncated version of an ideal spike and the nozzle resembles a spike hence called as aerospike nozzle. Due to its ability to adjust the environment by altering the outerjet boundary, the nozzle delivers better performance compared to present day bell nozzle and the very high ratio nozzle can also operate efficiently and safely at sea level. It is designed for 20 bar pressure ratio. To improve the performance of aerospike nozzle for various conditions, initially a model is created then optimisation is carried out which is designed by software CATIA and the flow behaviour is analyzed by CFD software called ANSYS.

PROJECT: Fluid Flow Analysis Around Supersonic Intake.

Description: The supersonic intake is used for the ramjet engine, which operate at supersonic domain. Accordingly, CFD simulations will be carried out to study the aerodynamic flow characteristics of an air-intake. The analyses will involve supersonic external and internal flow-field around the walls of the intake placed on the flat plat. The methodology to evolve the intake configuration will be carried out by study the shock-shock interaction, boundary layer-shock interaction phenomenon. The effect of wall thickness and the gap between walls will be study. The geometrical shape of the upper wall of intake will be study by taking in account the shock occurs due to the ramp angle. The three-ramp intake will be study using the shock meeting at one particular point.

ACHIEVEMENTS:

•Topped three semesters in my branch during my under graduation.

•Teamed in organizing “AERODYNE 2K19”, a technical fest conducted at Malla Reddy College of Engineering & Technology in the month of February, 2019.

•Student’s house leader for the house named “swami Vivekananda group” during my 9th and 10th class at my school.

PUBLICATION:

•Pulblished paper on Flow Field Analysis Around a Supersonic Intake(ICAB-2020) INTERNATIONAL CONFERENCE AERONAUTICS AND BEYOND(paper ID- ICAB125).

EXTRA-CURRICULAR ACTIVITIES:

•Participated in various workshops on “Catia” and “RC model aircraft designing” held at Malla Reddy College of Engineering & Technology.

•Volunteered in various service programs and events organized by Malla Reddy College Engineering & Technology.

PERSONAL SKILLS:

•Good communication and analytical skills.

•Zealous to learn more.

•Smart working.

•Positive thinking, confidence.

•Commitment and punctuality.

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