I am a quick learner and believes in learning from my past mistakes a
Resume:
SANJAYKANNA
**, *** ******, *********** *******, GOLLAMANGALAM POST,
GUDIYATTAM TALUK,VELLORE DISTRICT, TAMIL NADU - 635809 ********@*******.***
OBJECTIVE
I am keep to contribute to the success and growth of the organization by undertaking the challenging assignments and delivering timed results by applying best of my knowledge and skills. Experience
EDUCATION
SOFTWARE SKILLS
Catia V5 (medium).
• Expert in Microsoft office, with a focus on Excel.
• SolidWorks.
• ANSYS (Fluent).
• Image processing tool: Tracker.
• Hyper mesh .
PROJECT DETAILS
AREA OF INTEREST
FRESHER
ANNA UNIVERSITY / PARK COLLEGE OF ENGINEERING AND TECHNOLOGY, COIMBATORE B.E / AERONAUTICAL ENGINEERING
7.5
2016 - 2020
KONGU MATRICULATION HIGHER SECONDARY SCHOOL, DHARMAPURAI 12th STANDRAD / TAMILNADU STATE BOARD
75%
2014-2016
THIRUVALLUR HIGHER SECONDARY SCHOOL, GUDIYATTAM
10th STANDRAD / TAMILNADU STATE BOARD
70%
2014
NUMERICAL ANALYSIS OF PROTRUSION
EFFECTS OVER AN EPPLER-387
Need of micro aerial vehicles and Unmanned Air Vehicles is increasing due to military, defense and civilian requirements. These vehicles fly at very small Reynolds numbers and have to move in confined spaces with a bare minimum speed, to achieve high lift coefficient is the main concern. The main focus of this research paper is to carry out the computational analysis and study the unsteady flow over E387 aerofoil with right angle circle protrusion at the Reynolds number 105. The location of the protrusion is 30%c, with three different heights of protrusion 1.4mm, normal to the surface of the aerofoil. Geometric modeling and grid generation are created using the CFD software and numerical analysis carried out using CFD Software at various angle of attacks ranging from 00 to 160 with 20 intervals. Numerical validation has done and compared. The results obtained from the research work is recommend that for smaller protrusions the lift and drag coefficients are unaffected in the low angle of attacks while the lift characteristic is significantly improved at the higher angle of attacks. 1.Propulsion.
2.Aerodynamics.
3. Structures.
4.Computational Fulid dynamics
INTERNSHIP
CONFERENCE
DUTIES AND RESPONSIBILITIES
HOBBIES
STRENGHTS
DECLARATION
5.Codeing
6.Website creation
• A Five days implant training (10-12-2017 – 14-12-2017) at Kaashiv infotech.
• A Nineteen days Internship (18-06-2019 – 06-02-2019) at CRI Pumps (Tuff Pumps).
• Aero India 2019 International Seminar organized by Gas Turbine Research Establishments (GTRE), DRDO, Ministry of Defence, Govt. of India, C.V Raman Nagar, Bengaluru – 56009, Karanataka. Held on 18-02-2019 – 19-02-2019.
• Student volunteer at National Level Seminar held at Park College of Engineering &Technology. Organised by Tamil Nadu State Council for Science & Technology on 08-02-2019.
• Playing Cricket, Batmittion, Chess.
• Watching & Reading histories of Great Peoples,Politics&Comics.
• Video, Photo Editing.
• Good communication and Managements skills.
• Good team player and work under pressure.
• Dedicated and very decision maker.
• Able to handle multiple assignments.
I hear by declare that all information said above is true to the best of my knowledge and belief.
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