Hypermesh Ansys Cfx
Resume:
RESUME
CH. VSNS GOPIKRISHNA
PRAKASH NAGAR,
NARASARAOPET, GUNTUR.
ANDHRAPRADESH-522601
E-MAIL ID: **************@*****.***
Mob: +91-972*******
CAREER OBJECTIVE:
To strive for excellence and seek every opportunity to enhance my skills and abilities in areas of teaching interest to the best in the interest of the organization as well as self-enhancement.
EDUCATIONAL QUALIFICATION:
Examination
Discipline/
Specialization
School/college
Board/University
Year of Passing
Percentage of Marks
MTECH
AEROSPACE PROPULSION TECHNOLOGY
VTU CPCGS
VTU CPCGS
2016
76
BE
AERONAUTICAL ENGINEERING
Achutha Institute Of Technology
VTU BELGAUM
2014
60
Intermediate
MPC
Board of Intermediate
Board of Intermediate
2008
69
S.S.C
SSC
Board of Andhra Pradesh
Board of Andhra Pradesh
2006
77
SOFTWARE PROFICIENCY:
Certificate Courses : Hypermesh,Ansys CFX
Office Applications : Word, Excel, Power Point
Areas of Teaching interest:-
●AeroDynamics
●Gas Dynamics
●Propulsion
●Aircraft performance
Work Experience
●GUEST FACUILTY: IN APLIED MECHANICS MNNIT ALLAHABAD (CENTRAL GOVT) from 2017 January to May 31 2018.
●Worked under Internship program at DRDO for 4 months as a part of M tech course
Project Details -M TECH
Project Title : STUDY OF OFF DESIGN PERFORMANCE OF RADIAL TURBINE FOR A TURBOCHARGER
Company Name : GAS TURBINE RESEARCH ESTABLISMENT DEFENCE RESEARCH AND DEVELOPMENT ORGANISATION.
Duration : 6 MONTHS
Guided by : INTERNAL: DR. BASAWARAJ (ASSOCIATE PROFESSOR) EXTERNAL: Mr. S . V. RAMANA MURTY (SCIENTIST ‘G’, TECHNICAL DIRECTOR TURBINE DIVISION GTRE, DRDO, BANGALORE)
Project Description:
Turbocharger is an exhaust device used in automobiles. This device is used to boost engines power output by using waste exhaust gases. The goal of present thesis is to determines the study of off design Performance of radial turbine. At initial stage mean line analysis has used to determine the performance parameters. The radial turbine consists of turbine wheel and volute. The meshed data in ICEM-CFD is given by the organization. The software which is carried in this project is ANSYS CFX. The case set has done in CFX pre, solved in CFX solver and post processing is in CFX post. After the post processing data has collected and characteristics are generated for different speeds and pressure ratios for obtaining off design performance. Finally, theoretical values are compared with ANSYS CFX calculations.
PROJECT DETAILS :- BE
Project Title : “DESIGN &DEVELOPMENT OF PRESSURE SWIRL SPILL RETURN ATOMIZER FOR SMALL GAS TURBINE ENGINE
APPLICATIONS”
Company Name : Hindustan Aeronautical limited (HAL)
Duration : 6 months
Guided by : INTERNAL: DR. MR. RAVISHANKAR KALLIGUDD EXTERNAL: MR. V. REDDY
Project Description : software’s used in our project are “NX UNIGRAPHICS” & “MATLAB”. The project describes outlines the complete detail of experimental setup, which includes the incorporation of penetration length measurement along with spray cone angle, mass flow rate and Sauter mean diameter. Geometry of combustion chamber and methods for calculation of penetrations are therefore essential to sound engine design. In gas turbine combustor, spray angle has strong influence on ignition performance, flame blowout limits and the pollutants emission of unburned hydrocarbons and smoke. We have designed the pressure swirl spill return atomizer in “NX UNIGRAPHICS” and analyze the design efficiency of pressure swirl spill return atomizer by using “MAT LAB- The language of Technical computing.
PERSONAL TRAITS:
Team spirit and work commitment
Fast adaption to work in multicultural environments
Creative and adaptable
Ability to work under pressure
PERSONAL PROFILE:
Name : CH VSNS GOPIKRISHNA
Father’s Name : CH. ANNAPURNAIAH
Nationality : Indian
Gender : Male
Date of Birth : 12-07-1991
Permanent Address : #12-17-23/12,
Prakash Nagar
Narasaraopet, Guntur
Andhrapradesh-522601.
DECLARATION:
I hereby declare that the above-mentioned details are true to the best of my knowledge.
Date : 03-06-2019 Yours sincerely,
Place: Bangalore Gopikrishna.CH
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