Staff Analyst, Methods

Responsibilities

• Perform detailed structural analyses of dynamic system components, including the rotor system, control system, and blades
• Evaluate static strength and fatigue life of critical structures using classical hand calculations and finite element analysis for both flight loads and ground load conditions
• Evaluate component life and dynamic response of dynamically loaded metallic and composite components subject to high and low cycle fatigue
• Author structural substantiation reports and other required technical documentation to meet program needs
• Support full scale component ground testing and flight testing, including test requirements, layout, instrumentation, and data reduction
• Develop best practices for structural analysis of critical aerospace structures
• Collaborate with the aerodynamics and loads & dynamics teams to design high performance propeller and rotor blades
• Collaborate with internal and external customers to ensure on-time delivery of data

Qualifications

• Required:
• Bachelor’s degree in aerospace engineering, mechanical engineering, or related field
• 5+ years of experience in design and analysis of critical aircraft structures
• Proficient in ANSYS, NASTRAN, or other FE software
• Knowledge of fatigue and damage tolerance of composites
• Knowledge of high cycle and low cycle fatigue in metallic components
• Ability to read engineering drawings and interpret CAD models
• CAD design experience (NX preferred)
• Strong technical, written, and verbal communication skills
• Experience in a fast-paced design environment
• Preferred:
• Master’s in aerospace engineering, mechanical engineering, or related field
• 10+ years of experience in design and analysis of rotorcraft dynamic systems, including rotors, controls systems, and propeller or rotor blades
• Background in ground and flight testing of critical composite aerospace structures
• Familiarity with FAA aircraft and/or rotorcraft loads and dynamics regulations (FAR Part 23, 27, 33, 35) and associated advisory materials
• Experience with static and dynamic loads derivation for fixed-wing vehicles and/or VTOL aircraft
• Ability to perform aeroelastic analysis on VTOL dynamic systems
• Prior involvement in FAA or military rotorcraft certification efforts
• Proficiency in Python and/or Matlab scripting

Pay

This position will require travel up to 10% to Archer facilities or supplier facilities.

At Archer, we aim to attract, retain, and motivate talent with the skills and leadership needed to grow our business. We drive a pay-for-performance culture and reward performance that supports the Company’s strategy. For this position, we are targeting a base pay range of $15,000 - $190,000. Actual compensation offered will be determined by job-related knowledge, skills, and experience.