HARDIK RAMANI

I

N DEPARTMENT OF THERMAL ENGINEERING

F Institute of Technology Nirma University, Sarkhej Gandhinagar Highway,

Ahmedabad, India, Pin-382481

O

R Name: Hardik Vallabhbhai Ramani

M

Address: Phase - 1,

A

Hinjewadi, Pune,

T LANGUAGES KNOWN

I Maharastra-411057

English

O Hindi

Phone: (M): 098********, 088********

Gujarati

N acoyv8@r.postjobfree.com

E-mail:

acoyv8@r.postjobfree.com

Q

U

PERSONAL DETAILS

A M.Tech: Institute of Technology, Nirma University (2013-15)

FATHER’S NAME: V.M

PPI: 8.1 (Till 3rd Semester)

(Thermal

L Ramani

Engineering)

I

MOTHER’S NAME:

B. Tech: U.V. Patel college of Engineering, Ganpat

F University, Mehsana (2008-2012) Ranjanben V. Ramani

I Score: 70.38%

NATIONALITY: Indian-

C HSC: Sarveshwar School, Rajkot, Gujarat state board Hindu

(2008)

A MARITAL STATUS: Single

Score: 78.20 %

T D.O.B: 18th May, 1991

SSC: APS High School, Gondal, Gujarat state board

I (2006) HOBBIES

O Score: 89.00%

Reading

N Social Networking

S Playing Cricket

COMPUTER PROFECIENCY

S

CFD software: Fluent 14.5,Ansys 14.5,ICEM CFD, Gambit 2.4.6

K

CAD software: NX 8.0,Pro-Engineer

I

Heat Exchanger Software: HTRI

L Numerical Computational Package: scilab 5.3.3

L M.S Office, Internet, Latex

Programming Language : C++,ANSI C

S

SOFT SKILL

Adaptable and a quick learner with skills to work under pressure

Focused and goal driven with strong work ethics, continuously striving for improvement

coupled with commitment to offer quality work

P

R B.TECH PROJECT

O PROJECT TITLE

J Quality Control by Reducing Rejection due to Chip Impression

E

PROJECT DESCRIPTION

C

T At MAHINDRA GEARS & TRANSMISSION PVT.LTD.RAJKOT

Find out causes behind chip impression by collect & analysis the data by checking

D

amount of rejection within time duration. Then using Pareto chart & cause effect

E

diagram, find out causes behind it & take possible action to improve it.

T

A

I

L

P M.TECH PROJECT

R PROJECT TITLE

O Design and CFD analysis of Throat Cooling System for Hypersonic Wind Nozzle

J

PROJECT DESCRIPTION

E

C At ZEUS NUMERIX PVT.LTD, PUNE

T Carried out detail design by using empirical correlations and estimated heat flux caused

by hypersonic flow in nozzle for Mach number 5 and 6.5.The estimated heat flux is

D

compared with CFD result and validated.

E

For high Mach number the cooling of throat of hypersonic nozzle is required. The

T

conjugated heat transfer analysis is performed using Fluent 14.5.The prepossessing is

A

carried out in Ansys Workbench and ICEM CFD. Flat plate analysis has been used for

I estimation thermal property in side cooling channel.

L

The heat flux developed by hypersonic flow wad estimated using Eckert’s reference

temperature method and Bertz correlation. The c++ code of above two methods were

prepared by me.

E

X Industrial Experience:

P I have four month experience at G M Engineering, Rajkot. The company is well known in

E Industrial valve manufacturing industry.

R Vocational Industrial Training:

Zeus Numerix,Pune

I

(Hypersonic Wind Tunnel Base Nozzle Design & CFD Analysis)

E P.M. Diesels Pvt. Rajkot

(Assembly of Diesel Engine & Tractor)

N

Mahindra Gears & Transmission Pvt. Ltd. Rajkot

C (Gear Manufacturing)

E

Industrial Visit:

Adani Port and SEZ, Mundra, Gujarat

Adani Power Plant, Mundra

Sardar Sarovar Power Plant, Narmada, Gujarat

Utran Power Plant,Surat

Hitachi home appliance, Ahmedabad

Blue Star India, Bharuch, Gujarat

Jyoti CNC Ltd.,Rajkot, Gujarat

I hereby declare that the information furnished above is true to the best of my

knowledge.

HARDIK V. RAMANI

Place: Pune

Date: 26-03-15

Contact this candidate