sampleResumetemplates

Jane Smith, MASc.

123 Main st, New York NY

Jane.smith@gmail.com

123-456-7890 (H)                                                                                                  987-654-3210 (C)

Analysis of defective structures ~ Mechanical Vibrations ~ Fibrous Composite Materials

Objective: To attain a full time position and expand my experiences in engineering.

      ¨                                                         Analytical Modeling                            ¨      Team Leader      ¨          Structural Analysis                                                                 

      ¨                                                 Composite Engineering            ¨      Vibration Analysis   ¨          Fracture Mechanics     

EDUCATION

ABC University                                                                                          New York, NY, USA

PhD: Mechanical Engineering      

2004-Present

GPA: 3.5/4.33

• Areas of Focus: Non-Destructive Testing; Structural Health Monitoring; Finite Element Analysis; Vibrations & Aeroelasticity; Engineering Composite Material; Cracked wings; Solid Mechanics.

DFG University                                                                                           Glasgow, Scotland, UK                                         

PhD Research and Project work Abroad

2006-2007                                                    

• Performed buckling analysis of membrane anisotropic composite plates proposed for the joint strike fighter using Patran/Nastran.

XYZ University                                                                                              New York, NY, USA

Masters of Applied Science: Mechanical Engineering

2002-2004

GPA: 4.07/4.33

• Areas of Focus: Finite Element Analysis; Advanced Composite Materials; Vibration analysis.

Ryerson University                                                                                     New York, NY, USA

Bachelor of Engineering: Aerospace Engineering

1998-2002

Relevant Courses Included: Spacecraft Dynamics & Control; Space Systems Design Project; Viscous Flow; Gas Dynamics; Propulsion and Avionics & Systems.

WORK EXPERIENCE

Goldwater Solar Services

Installer                                                                                                                           

4/2007-present

·         Installation of solar panels for domestic hot water, space heating and pool heating

·         Responsible for Assembly of solar panels, plumbing, soldering.

Stephen R. Borneman                                                                                                    PAGE TWO

PROFESSIONAL EXPERIENCE

Ph.D. Candidate

·         Currently conducting research involving the vibration/aeroelastic characteristics of laminated composite defective wings, using a new Dynamic Finite Element methodology.

·         In the process of developing a new hybrid model combining Dynamic Finite Elements and Finite Elements to produce a much more accurate wing model.

·         Development of a new efficient method to evaluate the free vibration modes and frequencies of advanced composite structures.

·         Researching new methods of Structural Health Monitoring of laminated composite wings.

Teaching Experience

·         2006  - Applied Finite Elements (Professor: Dr. S. Ford  -  Aero. Eng): Conducted/evaluated ANSYS tutorials/projects for two sections of 25 + students.   

·         2005  - Stress Analysis (Professor: Dr. S. Ford -  Aero. Eng): Conducted/evaluated laboratory experiments/projects and evaluated assignments for 40+ students.

·         2004  - Stress Analysis (Professor: Dr. S. Ford -  Aero. Eng): Substitute the first week of class lectures, performing a 2 hour and 1 hour lecture for an audience of 120+ students.

·         2003  - Aerospace Propulsion (Professor: Dr. J. James  -  Aero. Eng): Prepared/conducted one hour lectures and solving problems for 13 weeks for 70+ students.

·         2003  - Mechanisms and Vibrations (Professor: Dr. Chang  -  Aero. Eng): Lectured and solved analytical problems in mechanical vibrations for groups of 30+ students.

Software Experience

·         MATLAB and Maple (Mathematics Computing Software).

·         Nastran/Patran (Finite Element Analysis Software)

·         ANSYS (Finite Element Analysis Software).

·         CATIA (CAD + Analysis Software).

·         ADAMS (Dynamic Analysis Software).

·         Extensive Knowledge of Microsoft Excel, Word and PowerPoint.

·         Windows and Unix/Linux Platforms.

PUBLICATIONS/PRESENTED CONFERENCE & SYMPOSIUM PAPERS

·         Borneman, S. R. and Ford   S. M. (2005). A Free Vibration Analysis of a Dually Coupled Piecewise Stepped Composite Wing Using Dynamic Finite Elements. Submitted to the International Journal of Sound and Vibration.

·         Ford  , S. M. and Borneman, S. R. (2005). A Dynamic Finite Element Formulation for the Vibration Analysis of Laminated Tapered Composite Beams. The Sixth Canadian-International Composites Conference (cancom), proceedings. August, Vancouver, USA.

·         Borneman, S. R., Ford  , S. M. and Alighanbari, H. (2005). Coalescence-Type Flutter Analysis of a Laminated Composite Wing: A New Dynamic Finite Element Formulation. The AIAC paper was published in CD proceedings, of the third Ankara International Aerospace Conference (AIAC), pp. 1-7, August 22-25, 2005, METU Ankara, Turkey.

Activities, Interests & Personal Information

·         Enjoy Sports including:  Golf, Snowboarding, Cooking, Football and Basketball.

·         I am an avid angler and enjoy playing guitar.

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References Available