An Overall 8 Yrs of experience with 4 yrs in the FEA / STRESS Analysis & 4.0 years of industrial & academic research experience. Possess a good understanding in the areas of CAD/CAE and FEA, STRESS ANALYSIS, COMPOSITE MATERIALS Linear/Non-Linear Static, Dynamic Analysis, Thermal Analysis, Piezoelectric Analysis by way of projects execution. Executed significant projects related to Tire Design & Analysis, Airframe Stressing in FE software/hand calculations, Acoustic analysis, Contact Analysis, Polymer Technology. Equally posses MS Word, MS Excel, MS PowerPoint, Documentation / Report Preparation & Presentation skills.
Current Experience
Pursuing PhD in Mechanical Engineering - Systems & Design with research work based on Engineering / Virtual simulation. Hold an appointment as “Teaching Assistant” for Capstone Design at University of Kentucky, Lexington, KY, USA. Current Research focuses on “FE Modeling & Characterization of CNT”- using ANSYS 12 & ABAQUS 6.9 EF
Previous Experience
Worked as Senior Analysis Engineer (CAE) at CADES Digitech Pvt. Ltd, a reputed engineering services company at Bangalore, Starting March-2006, till Dec 2009
Projects executed with CADES Digitech Pvt Ltd include:
(i) Design & FE Analysis (Non-linear static & Buckling) of Filament Wound Composite Motor Casing using CADWIND/ABAQUS/ MARC/ NASTRAN.
(ii) Hydraulic and Fuel line Transport Element Analysis of Boeing 787 - Dream liner using NASTRAN/PATRAN.
(iii) Design and FE Analysis of Light Truck Automotive Tire LT265/70R16 to validate its performance under given test conditions of Inflation and Rated Load using ABAQUS 6.7 & Hypermesh.
(iv) Modeling and simulation of Piezo operated MEMS switches using SMART Materials concepts in ANSYS & ABAQUS.
(v) Acoustic analysis of an Automotive Start Control Unit in SYSNOISE.
(vi) Stress hand calculations involving static strength checks for Empennage Skin Panel of SARAS T-Tail Aircraft.
My Education
Pursuing PhD in Mechanical Engineering - Systems & Design
Hold a Master of Technology (M.Tech) in Machine Design
Hold a Bachelor of Engineering(BE) in Mechanical Engineering
Hold a Diploma in Mechanical Engineering
My Skills, Certifications, Licensures
CAD/Simulation : AutoCAD, CADWIND (for Filament winding)
FE Pre / Post Processors: HYPERMESH 7.0, ABAQUS/CAE, MSC PATRAN
FE Analysis Solvers : ABAQUS 6.9EF, ANSYS 12.0, MSC NASTRAN, SYSNOISE, MSC MARC / MSC MENTAT
Programming tools : FORTRAN, MATLAB & SIMULINK.
1 Johnson Joseph
2 Master of Technology in Machine Design
FEA Stress Analysis
(Currently pursuing PhD in Systems & Design –University of Kentucky, Lexington, KY, USA)
8 Years of Experience in the Mechanical/Aerospace Engineering
Objective:
Seeking a better position in the challenging work environment of CAE catering to Aerospace, Automotive and Heavy Engineering Industry to actively contribute to the growth and development of the organization where my analytical, technical skills and practical experience could be utilized to the fullest extent and in the process, gaining more knowledge and experience to achieve my career objective of being in a responsible position.
Professional skills: An Overall 8 Yrs of experience with 4 yrs in the FEA / STRESS Analysis & 4.0 years of industrial & academic research experience. Possess a good understanding in the areas of CAD/CAE and FEA, STRESS ANALYSIS, COMPOSITE MATERIALS Linear/Non-Linear Static, Dynamic Analysis, Thermal Analysis, Piezoelectric Analysis by way of projects execution. Executed significant projects related to Tire Design & Analysis, Airframe Stressing in FE software/hand calculations, Acoustic analysis, Contact Analysis, Polymer Technology. Equally posses MS Word, MS Excel, MS PowerPoint, Documentation / Report Preparation & Presentation skills.
Tool Knowledge
CAD/Simulation : AutoCAD, CADWIND (for Filament winding)
FE Pre / Post Processors: HYPERMESH 7.0, ABAQUS/CAE, MSC PATRAN
FE Analysis Solvers : ABAQUS 6.9EF, ANSYS 12.0, MSC NASTRAN, SYSNOISE, MSC MARC / MSC MENTAT
Programming tools : FORTRAN, MATLAB & SIMULINK.
Current Job Profile:
Pursuing PhD in Mechanical Engineering - Systems & Design with research work based on Engineering / Virtual simulation. Hold an appointment as “Teaching Assistant” for Capstone Design at University of Kentucky, Lexington, KY, USA. Current Research focuses on “FE Modeling & Characterization of CNT”- using ANSYS 12 & ABAQUS 6.9 EF.
Journal Publications & Conference Presentations:
Johnson Joseph, S Raja and Y Charles Lu “Finite Element Analysis of Piezoelectric Composite Actuators” SAE Int. J. Mater. Manuf. June 2011 4:328-339; doi: 10.4271/2011-01-0218
Presented the above paper at the SAE World Congress - APR-2011, DETROIT, MI, USA
Yuebin Lu, J. Joseph, M. R. Maschmann, D. C. Foster, J. Baur “Large-Displacement Indentation of Vertically Aligned Carbon Nanotube Arrays” International Symposium on Plasticity and Its Current Applications ,Jan 3-8 ,2012, San Juan.
Current Academic Performance: Achieved a CGPA 3.8/4.0 from spring’10 to Fall’11
Company last worked: CADES Digitech Pvt Ltd. www.cadestech.com
Worked for a leading Engineering-Services company at Bangalore, INDIA involved in executing projects related to Consulting, R&D services to Aerospace, Defense and Automotive Industry.
Experience Summary of last held job:
Worked as Senior Analysis Engineer (CAE) at CADES Digitech Pvt. Ltd, a reputed engineering services company at Bangalore, Starting March-2006, till Dec 2009
Projects executed with CADES Digitech Pvt Ltd include:
(i) Design & FE Analysis (Non-linear static & Buckling) of Filament Wound Composite Motor Casing using CADWIND/ABAQUS/ MARC/ NASTRAN.
(ii) Hydraulic and Fuel line Transport Element Analysis of Boeing 787 - Dream liner using NASTRAN/PATRAN.
(iii) Design and FE Analysis of Light Truck Automotive Tire LT265/70R16 to validate its performance under given test conditions of Inflation and Rated Load using ABAQUS 6.7 & Hypermesh.
(iv) Modeling and simulation of Piezo operated MEMS switches using SMART Materials concepts in ANSYS & ABAQUS.
(v) Acoustic analysis of an Automotive Start Control Unit in SYSNOISE.
(vi) Stress hand calculations involving static strength checks for Empennage Skin Panel of SARAS T-Tail Aircraft.
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