1. Mohd
Azhar 07207871993,09700745184
Mohd.azhar@live.com
Linkedin.com/mohd-azhar
14-1-129/27/15PPADMAVATHI NAGAR
BORABANDA HYDERABAD-500018
CONTACT
To join an organization that gives me an opportunity to showcase my designing skills
and also helps me gain practical exposure in designing sector.
GOAL
EDUCATION
Master In Machine Design (72%)
Auroras Scientific Technological and Research Academy, HYDERABAD
Affiliated to JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY
HYDERABAD
Bachelor in Aeronautical Engineering (68%)
Maheshwara Institute of Technology, MEDAK
Affiliated to JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY
HYDERABAD
Diploma in Manufacturing and Product Design
Alison.com
Board of Intermediate (64.7%)
Sultan Ul Uloom Junior College, HYDERABAD
Board of Secondary Education (73%)
Nagar Juna High School, HYDERABAD
2014
2013
2010
SKILLS
Teamwork
Communication
Self Motivated
Leadership
2008
2016

2. Mohd
Azhar 07207871993,09700745184
Mohd.azhar@live.com
Linkedin.com/mohd-azhar
14-1-129/27/15PPADMAVATHI NAGAR
BORABANDA HYDERABAD-500018
CONTACT
EXPERIENCE
GIS Engineer
Shraddha Technologies
2016November
2014 – May 2015
CERTIFICATIONS
● AUTOCAD (CANTER CADD CENTRE, AMEERPET)
● CATIA V5 (CANTER CADD CENTRE, AMEERPET)
● ANSYS APDL (CANTER CADD CENTRE, AMEERPET)
● MS OFFICE (NI-MSME, YOUSUFGUDA)
● UG NX 9.0 (DESIGN TECH SYSTEMS, BANJARA HILLS AND
SIEMENS)
● AcuSolve, AcuConsole, AcuFieldView (AEROTRIX,
BANGALORE)
T
IFICATIONS
PROFESSIONAL ATTRIBUTES
● A high standard of professionalism in my work
● The ability to remain calm and objective in all situations
● The ability to quickly identify and resolve client problems
● Able to work autonomously and in a team environment
● A good sense of humour and the willingness to be part of a team
October2015–
December 2015
Internship
Design Tech System
June 2016–
September
Internship / Academic Project
Frugal Technologies Private Limited

3. SS
Mohd
Azhar
CONTACT
14-1-129/27/15PPADMAVATHI NAGAR
BORABANDA HYDERABAD-500018
07207871993,09700745184
Mohd.azhar@live.com
Linkedin.com/mohd-azhar
PERSONAL PROFILE
NAME : MOHD AZHAR
FATHER NAME : MOHD GHOUSE
D O B : 02-07-1993
AGE : 23 YEARS
MARITAL STATUS : UNMARRIED
GENDER : MALE
RESIDENTIAL ADDRESS: 14-1-129/27/15P PADMAVATHI NAGAR BORABANDA
HYDERABAD
NATIVE : HYDERABAD
LANGUAGE KNOWN : ENGLISH, HINDI, TELUGU
EXPECTED SALARY : AS PER COMPANY NORMS
CELL NO : 7207871993, 9700745184
PASSPORT NUMBER : L6530074
I do here by confirm that the information furnish above is true to the best of
my knowledge and belief
DATE:
PLACE:
(MOHD AZHAR)
DECLARATION

4. Mohd
Azhar
CONTACT
14-1-129/27/15PPADMAVATHI NAGAR
BORABANDA HYDERABAD-500018
07207871993,09700745184
Mohd.azhar@live.com
Linkedin.com/mohd-azhar
MTECH PROJECT
Aerodynamic Static Structural Analysis of VAWT
In this project a model for the evaluation of the energy performance and
aerodynamic forces acting on small straight bladed Darrius type vertical axis wind
turbine depending on blade geometrical section has been developed, based on a
analytical code coupled to a solid modelling software’s which was linked to FEA (Finite
element analysis) & FVM (Finite volume method) of structural and CFD code for
calculation of rotor performance.
Here the design of VAWT with NACA 0021 airfoil which is able to generate the
max power of 63.71watt at velocity of air 6.0554m/s is an optimal design at rated 75
RPM. The above design has been studied with aerodynamic static structural analysis
using ansys 16.0 which results to safe design without any potential failure in model.
The straight three bladed vertical axis wind turbine rotor is with 310 angle of attack in
order to improve the performance of rotor. By changing rotor maintain the height and
diameters of rotors the weight of rotor are significantly increase the weight without
compromising the performance of the rotor. For this purpose aerodynamic static
structural analysis in ANSYS of a straight blades VAWT rotor has been undertaken. Due
to limitations on experimentations, aerodynamic approach has been used to quantify
the wind load on the blades.
The main aim of this project is to design and analysis of an efficient Vertical Axis wind
turbine, on the further application of this loads, structural behaviour of the rotor is
obtained for a pre-determined set of operating conditions. The result form the analysis
is compared with pre-existing once for the purpose of validation.
PAPER PUBLISHED
PAPER TITLE : Aerodynamics Static Structural Analysis of VAWT
JOURNAL : INTERNATIONAL JOURNAL OF SCIENTIFIC ENGINEERING AND
TECHNOLOGY RESEARCH
PUBLISHED MONTH : SEPTEMBER 2016
PAPER (JOURNAL) LINK: http://ijsetr.com/issue.php?issue=ISSUE%2029&volume=Volume5

5. Mohd
Azhar
CONTACT
14-1-129/27/15PPADMAVATHI NAGAR
BORABANDA HYDERABAD-500018
07207871993,09700745184
Mohd.azhar@live.com
Linkedin.com/mohd-azhar
TECHNICAL SEMINAR
MAIN PROJECT
MINI PROJECT
Design and Analysis of Radial Turbine
Flow behaviour is observed inside the turbine at different guide vane angles and
got the maximum radial inflow turbine efficiency for all cases and comparison is
done between theoretical efficiency. Characteristic curve is verified for all the
different guide vane angles. For every case inlet velocity is changed as 10m/s,
7m/s, 4 m/s. Using CATIA V5 and ANSYS APDL software are used.
In a radial inflow turbine the flow enters the nozzle blades in the radial
direction (or in the case of a swirl generating volute in the tangential direction).
The flow enters the rotor blades in the radial direction, is turned in the rotor
passage and exits along the axis of rotation.
Radial inflow turbines are suitable for many applications in ship, aircraft,
space power systems, and other systems where compact power sources are
required. They are also used in air liquefaction plants and have been employed in
power generation units providing up to 2 megawatts of power for a variety of
industrial applications, aiming to replace heavy diesel engines. Radial turbines
have several advantages over an axial turbine..
Fabrication of Electronic Igniters
Electronic igniters are used as spark plugs which by increasing the
temperature it starts the engine by the use of battery attached to it through
wires, so that it reduces the mechanical energy for starting the engine
Anti icing System of Aircraft
Anti icing is a system which uses anti icing liquid over the surface of the
aircraft so that there is no ice formation for a certain period of time. It is applied
before the operation of the aircraft.
Anti-icing of aircraft is accomplished by applying a protective layer, using a viscous
fluid called anti-ice fluid, over a surface to absorb the contaminate. All anti-ice fluids
offer only limited protection, dependent upon frozen contaminant type and
prevailing weather conditions. A fluid has failed when it no longer can absorb the
contaminant and it essentially becomes a contaminant itself. Even water can be a
contaminant in this sense, as it dilutes the anti-icing agent until it is no longer
effective Preemptive, turned on before the flight enters icing conditions Includes:
thermal heat, prop heat, pitot heat, fuel vent heat, windshield heat, fluid surface
deicers, and propeller anti icing, wind shield anti icing, electro impulse deicing and
boots