Trevor Anderson is a Blade Design Engineer at Lockheed Martin since September 2022, with prior experience as a Structural Design Engineer at Spirit AeroSystems, where design efforts for the Bell V-280 Aft Fuselage involved collaboration with Stress Engineers and Manufacturer Engineers. Earlier roles included serving as a Student Ambassador Leader and Research Assistant at Oklahoma State University, where mentorship and research on force generation over revolving wings were key responsibilities. Trevor also gained valuable experience as a Design & Stress Engineering Intern at Spirit AeroSystems, focusing on fastener patterns and critical stress analysis while utilizing CATIA v5 for design optimization. Trevor holds a degree in Aerospace and Mechanical Engineering from Oklahoma State University, completed in 2021.
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