Telecommute Computer Science Nasa Jobs in Oklahoma

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).