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About the Job
Overview
You will play an integral role in building knowledge of one of the most unique and important subsystems on the Joby aircraft, its propeller system. You will use industry-standard tools for rotorcraft analysis to model and analyze our design. You will create aeromechanical data to support certification and development activities. You will validate the models against experimental and flight test data. You will engage with a variety of teams, including loads, aeroelasticity, aeroacoustics, noise & vibration, flight dynamics, airframe and actuators, flight testing, ground testing, certification, and more. The role requires a self-driven individual with the skills and desire to advance the state of the art of rotor dynamics for eVTOL aircraft. A strong mathematical background with a firm grasp on the fundamentals of the physics involved is necessary, with demonstrated performance as a self-starter.
Responsibilities
Develop and maintain aeromechanical models of the propeller system using RCAS and higher fidelity CFD/CSD methods
Perform aeroelastic loads (static design and fatigue) and stability analyses of the propeller system
Create aeromechanical databases for the propeller system
Design flight, system, and subsystem tests for validation of rotor dynamics models
Interpret test data to correlate and validate propeller aeroelastic models
Work closely with the propeller design team on modeling of aerodynamic and inertial loading of the blades and mechanisms
Required
M.Sc. in aerospace engineering, mechanical engineering, or a relevant discipline
3+ years' experience performing rotorcraft analyses or a Ph.D. in a related field
Strong fundamental grasp of rotor dynamics, aerodynamics, structural mechanics, finite-element analysis, multi-body dynamics
Experience with RCAS or similar comprehensive rotorcraft analysis tools and an understanding of its limitations
Proficient with computational analysis using tools such as Python, MATLAB, and Linux/Unix
Demonstrated self-starter with independent problem-solving capabilities
The ability to bring traditional and novel approaches to bear in the application of regulations, guidance material, and engineering specifications
Strong technical documentation skills and organization
Desired
Experience with high-performance computing
Ability to set up batch simulations using Linux/Unix tools and methods (bash, Python, Slurm/PBS)
Experience with and understanding of high fidelity CFD/CSD methods
Experience with flight and/or ground rotor dynamic testing methods and theory
Experience with propeller or rotorcraft product design and support
Compensation at Joby is a combination of base pay and Restricted Stock Units (RSUs). The target base pay for this position is $91,500 - $122,000/ yr. The compensation package will be determined by job-related knowledge, skills, and experience.
Additional Information
Joby Aviation is an equal opportunity employer.
About the Company

Joby Aviation
Joby Aviation develops a new generation of electric personal aircraft created to revolutionize personal mobility. Its strength is in composite airframe design and fabrication, aerodynamic analysis, high-performance electric motor development, and cutting-edge battery pack design, enabling clients to create a paradigm shift in transportation with safe, quiet, fast and affordable electric vertical takeoff.