To excel in the dynamic and developing field of Aeronautical with CFD and
by utilizing my technical and interpersonal skills and also to obtain a
position in your industry and to
achieve better utilization of my innovative thinks and hard work together
with your company goals.
B.E. Aeronautical Engineering completed in the year 2008 in Mohamed Sathak
Engineering college affiliated to Anna University,in first class with an
aggregate of 72%
H.S.C., Tamil Nadu State Board of Higher Secondary Examinations in the year
2004 with 75%.
S.S.L.C., Tamil Nadu State Board in the year 2002 with 85%.
CFD & FEA Skills:
Modeling : Gambit, Solid Works
Meshing : ICEM CFD, Gambit, TGRID
Analysis : Fluent, Icepak, CFX, Turbo grid, Star CCM+,
Ansys All packages (Work Bench), Autodyn.
Overall 4 years of experience in CFD & FEA
Company name : Extreme Mech Experts,
Period : June 3, 2008 to Jan 10 2011(2.5 yrs)
Designation : Wind Tunnel Design & Analyzer
High subsonic wind tunnel designed to achieve speed of 80 m/s with the mach
number of 0.8, contration ratio of the tunnel is
9:1,blower is used to suck the air into the tunnel,
Supersonic wind tunnel designed at Mach number of 1.2, with storage tank &
smoke generator is used to
identify the flow streamlines of the flow.
High supersonic wind tunnel designed at mach number of 2 with anechoic
Schileron apparatus, and shadow graphy system, storage tank and reservoir.
Also designed the test section for the wind tunnel according to need of
Handling Research projects on Industry sides, Ph.D, M.E, B.E Projects using
Company name : Mecavia pvt ltd, Chennai.
Period : Jan 16, 2011 to till date (1.5 yrs)
Designation : Project Engineer
Planning the procedures for the specific project
Estimating the time and cost of the project
Allocating the work to resources
Attending the client meeting
Title : Estimation of roll rate for LGB using Gambit- Fluent
Analysis roll rate for SUDARSHAN laser guided bomb at mach no. at 0.7, AOA
at 0- 90 degrees for canard deflection with step increase of 7.5 degree
Title : Numerical analysis of IC engine for variable combustion ratio using
Analysis to carry out for the various Combustion volume ratios, Ignition
time, fuel properties like Diesel, Bio-diesel, Jetrofoil.
Title : Numerical Analysis of Fuel Cells for Using Gambit-Fluent
Study carried out the losses at each bend of the fuel cell for desire
And determine the desired velocity and Pressure.
Title : Numerical Analysis of Rocket Engine Combustion Chamber Using GAMBIT-
Analysis of Rocket combustion chamber thrust for liquid propellants like
N2O4 (Nitrozentetroxide), UH2O5 (Dimethyl hydrazine & hydrazine hydrate)
using bell type nozzle.
Title : Numerical simulation of Aerofoil for high lift application using
CFD (GAMBIT -FLUENT).
Naca 65212 (6series) aerofoil which is used with high lifting devices as
slots & flaps
For shortest distance takeoff and landing purpose.
Title : Numerical simulation of flow over Autonomous Underwater Vehicle
(AUV) with propeller interaction
Analysis of flow over autonomous underwater vehicle with propeller
interaction under various latitude of pr conditions.
Title: Heat Transfer simulation of Turbine Blade. Using GAMBIT- MATLAB
Analysis of Turbine Blade heat transfer is carried to reduce the
temperature and increase the life of turbine blade. It also helps as how
turbine blade cooling is taking effect as by simulation.
Title : Numerical Simulation of Cyclone Heat Exchanger Using GAMBIT-FLUENT
Analysis of cyclone heat exchanger for various the size of the
particle,velocity,and time to track the particle reach out time of the
collector of holdup mass, when laden gas get pass out.
Title : Numerical analysis of Thermal spray gun for coating metal by using
Analysis of thermal spray gun which is used to coating metal with reaction
Title : Numerical analysis of Turbine Blade using Turbogrid, CFX& Ansys
Flow & structural analysis of turbine blade is carried out at 800 & 1200'C
for various high temp materials like Inconel600, Inconel718,
Udimet720, RR1000, Alloy 720 Li.
Title : Numerical Analysis of Explosive Welding Of Metals With And Without
Interlayer using ANSYS-AUTODYN
Analysis thermal explosive of welding, how the metal is welded when the
explosive taken with without interlayer of the metal like SS-Al, SS-Cu,
NEOGEL used for detonation, & to calculate the flyer plate velocity &
energy when explosion take place.
Title :-Numerical Analysis of Performance of Glass Fiber Reinforced Polymer
Wrapped Elliptical Columns by GAMBIT-ANSYS WORKBENCH
Analysis the performance of Glass Fiber Reinforced Polymer Wrapped
Elliptical column, for the various size of concrete, Young's modulus,
loads& number of wraps of GFRP is increased, and how the deformation takes
place and how much the elliptical column can withstand the applied load.
Title: Numerical Analysis of Aircraft Landing Gear for Gradual,
Sudden& Impact Load by ANSYS-WORKBENCH
Analysis stress, deformation on the landing gear when G-load, Impact load,
sudden load, gradual load on the landing gear at landing.
All project accompanied by data interpretation, analysis and technical
Date of Birth : 3rd Feb 1987
Father's Name : M.Sheik Ali
Nationality : Indian
Passport no : G9309754
Languages Known : English, Tamil.