EMAIL ID : firstname.lastname@example.org CONTACT NO: 990*******
Masters in Mechanical Engineering with 1 year experience in design and development of aerospace components. Insightful 3 years of experience in teaching and well conversant with Structural Subjects (Static, Fatigue, Strength of materials, FEM hand calculation).
•Analysis tools -, Ansys Workbench, Hypermesh, Nastran Patran.
• General software’s - Microsoft office and Microsoft Excel.
•Design and Development of aerospace components.
•Coordinating and guiding students final projects.
Organization: MVJ College of Engineering
Department: Mechanical Engineering
Duration: (Sep 2016 – Present)
Subjects Handled: FEM, Fracture Mechanics, Mechanics of Materials, Metrology, Design of Machine Elements I and II, ANSYS Lab.
Key Projects / Hands on Systems:
Guided project on “Design and Simulation of HAZMAT Truck Impact Safety System using ANSYS”.
Guided project on “ AStudy on the Crack Stopper for Enhanced Damage Tolerance Evaluation of a Fuselage Stiffened Panel”.
Guided project on “ Table Come Bed”.
Guided project on “ Design and Fabrication of VFM”.
Organization: National Aerospace Laboratory.
Department: STTD (Structures)
Duration: Aug 2015 to July 2016
Tool Used: MSC Nastran Patran
•Performing design change studies to optimize the design
•Modal analysis to evaluate Natural frequencies and Mode shapes of the system.
•Performing component failure analysis study, Low Cycle fatigue (LCF) calculations using SN curve.
•Validation and detailed design report and stress reports for review.
3.Evaluation of Damage tolerance evaluation of a crack stopper in a fuselage stiffened panel.
•Finite element model is generated in ANSYS & NASTRAN for stiffened panel.
•Linear static analysis to obtain the critical location for crack initiation in the stiffened panel.
•SIF variations with the progressive crack lengths are calculated and plotted.
•An L and Z Shaped stiffeners are introduced to make the structure damage tolerant.
•The Fatigue life estimation from the SIF variations using MATLAB coding.
Results:-Main purpose of the analysis is to find the critical stress location, crack growth in transverse direction & remaining residual life.
1.Design and optimization of Crack Stopper.
Optimizing the shape of crack stopper.
2.Design and fabrication of axial radial permanent magnet thrust bearing.
Works on the magnetic levitation concept.
3.Patch analysis test.
Theoretical calculation of the SCF.
Paper Presented In First International Structural Integrity Conference and Exhibition(SICE 2016), Organized By IIT Madras and IISC B ngalore.
Masters of Techn. (Engineering Analysis and Design) VTU, Belagavi
Bachelor of Engg. (Mechanical) VTU, Belagavi
o Date of Birth : 19th - Nov- 1992
O Languages Known : English, Kannada, Telugu and Hindi.
o Nationality,Gender : Indian, Female
o Address for Communication : #498,1stcross,Ambedkar Colony,Channasandra, BNG.
I hereby declare that the above furnished details are correct to the best of my knowledge
Place: Bangalore Akshitha G