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 ********@********.**.**
E-mail:
******.******@*****.***
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