Modelling Simulation Jobs in Oklahoma (NOW HIRING)

Indotronix is seeking : Onsite Job - Structural Analysis Engineer 4 Work Location: Oklahoma City, OK Duration: 12 Months Shift: First Start Time: 8:00 AM End Time: 5:00 PM Is Clearance Required To Start?: No Position Responsibilities: * Ensures compliance with methodology and processes for stress analysis, Durability & Damage Tolerance (DaDT) analysis, and finite element modelling in the accomplishment of work. * Performs Failsafe Analyses, durability life calculations, and determines Damage Tolerance for fracture critical parts. * Familiar with Single Flight Probability of Failure methods for determining fleet risk. * Verifies structural integrity by defining requirements for development of analytical methods, finite element models/simulations, and other analysis tools to develop the airframe structural environment, characteristics, and performance of the product. * Ensures USAF Aircraft Structural Integrity Program (ASIP) requirements are met for airframe analysis and validation. * Calculates inspection intervals for fleet aircraft based upon calculated crack growth rates. * Develops and uses various Finite Element Models for crack growth coefficients. * Understands proper application of loads in FEMs. * Understands industry best practices in airframe primary structure and load paths. * Supports product design and verifies structural integrity using analytical methods, finite element models/simulations, and other analysis tools throughout the product lifecycle. * Supports in-service products by investigating failures and analyzing improvements. * Develops analytical processes/tools to improve effectiveness, quality, and efficiency of repair development efforts. * Leads repair development, integration, and documentation of structural requirements to establish system design. * Works under minimal direction. Basic Qualifications: * Bachelor's, Master's, or Doctorate of Science degree from an accredited course of study in Engineering. * Ability to independently construct, execute, review, and manage structural finite element models in the area of Durability & Damage Tolerance (DaDT). * Expertise in Linear Elastic Fracture Mechanics. * Expertise with Paris Law and Spectrum Analysis. * Experience with crack growth analysis tools such as NASGRO, AFGROW, GROWTH, NASA/FLAGRO, or BEAS. * 10+ years of experience in structural analysis. * 10+ years of experience in fracture, fatigue, and/or Durability & Damage Tolerance (DaDT) analysis. * Strong written, verbal, and presentation skills. Preferred Qualifications: * Active U.S. Secret Clearance. * Familiarity with Boeing Books 1, 2, 3 & 4 with an emphasis on Durability & Damage Tolerance. * Experience with Hypermesh, StressCheck, Abaqus CAE, and/or Nastran. * Familiarity with Lifeworks. * Graduate-level or senior-level coursework in Fatigue & Fracture Mechanics. * Experience validating or verifying finite element model results. * Experience with structural design principles for aircraft primary structures, including fatigue, damage tolerance, corrosion, stress analysis, statics, material strength, material characteristics, and repair techniques. * Experience with Boeing Commercial Derivative aircraft primary structures, including commercial and/or military applications (737, 747, 757, 767, and 777). Education / Experience: * Education/experience typically acquired through advanced technical education from an accredited course of study in Engineering, Computer Science, Mathematics, Physics, or Chemistry (e.g., Bachelor's degree) and typically 9 or more years of related work experience, or an equivalent combination of technical education and experience (e.g., PhD + 4 years' related work experience, Master's + 7 years' related work experience).