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Senior Stress Engineer résumé example

Senior Stress Engineer résumé example — senior, written for United States, set in the Sterling design
Senior Stress Engineer résumé example, in the Sterling design

Twelve years of airframe and composite analysis, told through certification evidence that was accepted the first time.

Written for United States, at senior, in the engineering field, shown in the Sterling design. Every name, employer, address and number below is invented.

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Adrian Petrossian — Senior Stress Engineer

Wichita, KS

Stress engineer with twelve years on metallic and composite airframe structures, eight of them producing certification evidence for Part 25 programs. Owned the static and damage-tolerance substantiation for a composite wing-to-body fairing that the FAA accepted without a single finding. Appointed a Structures Designated Engineering Representative in 2024.

Experience

Senior Stress Engineer, Hollis Aerostructures · April 2021 – present

Structures group of eleven; owns substantiation for composite empennage and fairing assemblies.

  • Owned static and damage-tolerance substantiation for a composite wing-to-body fairing, accepted by the FAA with no findings across 340 pages of analysis.
  • Cut a bonded-joint margin review from six weeks to nine days by replacing hand checks with a scripted Nastran post-processor the group still runs.
  • Traced an in-service cracking report on 62 delivered shipsets to a fastener edge-margin shortfall and wrote the repair scheme that returned all 62 to service.
  • Removed 41 lb per aircraft from the empennage by re-laminating three skin panels while holding every margin above 0.05.
  • Mentors four engineers on composite failure criteria; two have since signed their first certification reports.

Stress Engineer, Whitmore Aero Systems · June 2017 – March 2021

  • Built and correlated a 1.2 million-element finite element model of a cargo-door surround, matching full-scale strain-gauge data within 6%.
  • Wrote 28 stress reports supporting a derivative type certificate, all accepted by the delegated authority on first submittal.
  • Automated margin-of-safety rollups across 9,000 elements, removing about 200 engineer-hours per analysis cycle.

Structural Analyst, Larkfield Composites · August 2014 – May 2017

  • Analyzed and tested 46 composite coupon and element configurations, building the allowables database two later programs were certified against.
  • Showed the bearing-bypass method then in use carried 22% of unnecessary conservatism, releasing capability that removed 14 fasteners per panel.

Education

  • M.S. Aerospace Engineering · University of Kansas · August 2012 – May 2014
  • B.S. Mechanical Engineering · Kansas State University · August 2008 – May 2012

Skills

  • Analysis: Classical hand analysis, Linear and nonlinear FEA, Damage tolerance, Fatigue and fracture, Composite failure criteria, Buckling and crippling
  • Tools: MSC Nastran, Patran, Abaqus, HyperMesh, NASGRO, Python
  • Certification: FAR Part 25 Subparts C and D, AC 20-107B, Static and fatigue test support, Stress report authoring, Repair dispositions

Certifications

  • Designated Engineering Representative — Structures — Federal Aviation Administration
  • Professional Engineer (Mechanical), Kansas — Kansas Board of Technical Professions
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