Loads and Dynamics Engineer, Air Vehicles

Job description

Job responsibilities

• Develop structural loads analysis for multiple air vehicles and systems to ensure structural integrity under various flight and ground conditions
• Generate and maintain integrated dynamics FEMs for multiple vehicles for use in loads derivation, aeroelastic flutter and other analyses
• Conduct aeroelastic and aeroservoelastic studies to predict and verify aircraft behavior
• Conduct flutter analysis to inform vehicle design and ensure flight safety
• Generate flight loads data in accordance with MIL and FAR specifications, such as FAR 23, 25, JSSG-2006, and other relevant standards
• Collaborate with design engineers to develop structural optimization strategies based on loads analysis results
• Prepare detailed technical reports and present findings to internal teams, management, and external customers
• Develop and perform dynamics testing, including vibration testing, modal testing, GVT, etc.

Job requirements

• Bachelor’s degree in engineering or applied physics with a focus in structures
• 5+ years of experience in a structures, dynamics or loads related role with high ownership and accountability for hardware outcomes
• Deep understanding of statics, dynamics, solid mechanics, materials science, finite element analysis and dynamic testing
• Proficiency in the use of FEMAP, Nastran or similar
• Proficiency in Matlab, Python, or similar for developing analytical models, data acquisition and automation
• Self-directed, results oriented, and capable of working in a dynamic environment
• Excellent time management, organizational, and communication skills
• Eligible to obtain and maintain an active U.S. Secret security clearance