Loads and Dynamics Engineer

General Atomics-posted about 2 months ago
$68,770 - $116,193/Yr
Full-time • Entry Level
Hybrid • Poway, CA
5,001-10,000 employees
Publishing Industries
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General Atomics Aeronautical Systems, Inc. (GA-ASI), an affiliate of General Atomics, is a world leader in proven, reliable remotely piloted aircraft and tactical reconnaissance radars, as well as advanced high-resolution surveillance systems. We have an exciting opportunity in San Diego, CA (Poway, CA) for a Loads and Dynamics Engineer in our Airframe Integrity Group. Under general supervision with limited review, this position is responsible for determining and developing effective approaches for resolving a wide range of difficult engineering problems. We recognize and appreciate the value and contributions of individuals with diverse backgrounds and experiences and welcome all qualified individuals to apply.

  • Responsible for supporting the design of new products, expanding capability to existing products, and integrating new payloads onto existing platforms.
  • Responsible for performing loads and dynamics analysis of aircraft components, assemblies, and systems.
  • Develop design and repeated loads for air vehicle flight, landing, and ground operations.
  • Flight Loads analysis includes the development of open and closed loop aeroelastic flight loads models, the calculation of aerodynamic and inertial loads across the aircraft.
  • Landing and Ground loads includes hand calculation methods, structural dynamics and explicit simulations of landings.
  • Dynamics analysis includes normal modes, frequency response, random vibration, and the development of vibration and shock environmental criteria.
  • Develop aeroelastic models for use in flutter and aeroservoelastic analysis.
  • Utilize ground vibration test data to correlate structural dynamics models.
  • Perform analysis by way of classical and computer methods, and develop new methodologies for load development.
  • Generate documentation to support design and airworthiness certification using MIL, STANAG, or FAR standards.
  • Typically requires a bachelors or masters degree in engineering or a related technical discipline from an accredited institution and two or more years of engineering experience with a bachelors degree. May substitute equivalent engineering experience in lieu of education.
  • Must have a general understanding of engineering concepts, principles, and theory with technical experience demonstrating the application of those concepts while ensuring safety and regulatory compliance.
  • Must possess the ability to understand new concepts quickly and apply them accurately throughout an evolving environment and organize work assignments to meet established timetables.
  • Good communication, computer, documentation, presentation, and interpersonal skills are required, as well as the ability to work both independently and as part of a team.
  • Must have the ability to perform FEA on composite airframes/structures.
  • Experience in the aerospace or related industry and with loads analysis and loads development experience is required.
  • Must be familiar with loads development, statics, dynamics, aerodynamics, stability and control, and vibrations.
  • Must be familiar with gusts, landing simulations, and flutter
  • Able to work extended hours as required.
  • Ability to obtain and maintain a DoD security clearance is required.
  • Working knowledge of panel codes, NASTRAN, or ABAQUS software is preferred.
  • Experience with aeroelastic loads development, closed-loop flight control systems, flutter, in-flight testing, and explicit time domain analysis for loads development is desirable.
  • Experience with Matlab, Excel, Visual Basic, panel codes, NASTRAN, ABAQUS, ZAERO, or other loads Loads and Dynamics software.
  • A working knowledge of JSSG, Mil-Spec, and FAA airworthiness requirements is advantageous.
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