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Hypermesh Ansys Cfx

Location:
Whitefield, New Hampshire, United States
Salary:
20000
Posted:
June 05, 2019

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Resume:

RESUME

CH. VSNS GOPIKRISHNA

#**-**-**/**,

PRAKASH NAGAR,

NARASARAOPET, GUNTUR.

ANDHRAPRADESH-522601

E-MAIL ID: ac9jfp@r.postjobfree.com

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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