Aircraft Stress Engineer
Location: Montreal, QC
Stress analysis and support for new primary /secondary aircraft structures. Perform analysis of aircraft structural designs including loads analysis and development of FE models. Knowledge of aircraft primary structures such as engine pylon, fuselage, pylon panels, ribs, engine fittings, fuselage skin panels, stringers and frames. Provide substantiation compliance reports, technical support and documentation of static strength methods, analysis, tests and engineering data. Experience with metallic and composite structures and knowledge of hand calculations and finite element techniques.
Desired Skills & Experience:
Previous related experience in stress analysis for aircraft structures. Experience with skin buckling and post-buckling analysis, crippling, joint analysis, fatigue and damage tolerance, crack growth, Bruhn, Roark, Niu, ESDU, etc. Familiar with FE post processing, NASTRAN, PATRAN, FEMAP, ANSYS and CATIA V5. B.Sc. /M.Sc. Mechanical /Aerospace Engineering with related experience.
Finite Element Analysis
Prime Source Management Inc.
100 King St. W., Suite 5700, Toronto, ON, M5X 1C7
P: 416-362-6222 | F: 416-362-4506
Email: hr @ prime-source.com
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