Kimberly Ferguson Cotter

Structural/Mechanical Engine at HARVARD INTEGRATIONS
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us****@****om
(386) 825-5501

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Nuku Doamekpor

Kimberly is a diligent and extremely hard worker. She studies until she understands the problem completely, in unafraid to ask for assistance when she doesn't. Her calm demeanor is always welcome to those around her. She is always willing to impart her knowledge to others and allows others to think analytically when helping. She is an extremely valuable asset to which ever company that has the pleasure of working with her

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Experience

    • United States
    • Manufacturing
    • 1 - 100 Employee
    • Structural/Mechanical Engine
      • Jan 2021 - Present

    • United States
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Structural Analysis Engineer
      • Jun 2010 - Apr 2014

      Structural Engineer/Stress Analyst Level 2 Feb 2013-April 2014 Boeing 737 MAX Moveable Leading Edge -Resized primary and secondary structure of 737-900ER for new performance and loading requirements Boeing 737 Moving Line -Redesigned existing structure to be functional for moving line production Intern Coordinator -Facilitated the summer engineering intern program for university students -Participated in college recruitment events at multiple universities Engagement of Women Engineers Team -Addressed problems of engineering attrition and recommended solutions to management Structural Engineer/Stress Analyst Level 1 June 2010-Feb 2013 Boeing 787 -9 Moveable Leading Edge -Analyzed Finite Element Models (FEM), static strength, and fatigue strength for new product development Boeing 787 -8 Sustaining Engineering & PSE (Production Support and Efficiency) -Consulted on and reviewed engineering design changes for metallic and composite structure -Researched recurring production concerns for cost savings improvements -Served as 6S focal to improve workplace efficiency and productivity Stress Engineering Intern May 2009-Aug 2009 Boeing 787 Leading Edge Program -Used PATRAN/NASTRAN Finite Element Analysis software to create and analyze structural load models -Designed new methodology for weight savings initiative to reduce flange thickness of wing leading edge ribs

Education

  • Iowa State University
    BS, Aerospace Engineering, French, NonDestructive Evaluation (NDE)
    2005 - 2010
  • EPFL (École polytechnique fédérale de Lausanne)
    Génie Mécanique, Science des Matériaux, Français
    2007 - 2008
  • South Dakota State University
    Master's degree, Engineering
    2020 -
  • University of Southern California
    Master of Science (M.S.), Aerospace, Aeronautical and Astronautical Engineering
    2011 -

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