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- Creation and/or modification of primary and secondary structural parts, assemblies, installations, and interface control models/documents.
- Contributing to developing, testing, and validating aircraft structural dynamics analyses.
- Assisting in creating system requirements, trade studies, statements of work, and test plans.
- Coordination with internal Integrated Product Teams (IPTs), with some interaction with external IPTs and suppliers.
- Bachelors degree in an engineering technical discipline such as Mechanical, Aerospace, or Aeronautical; 9 years experience with a Bachelors Degree or 7 years with a Masters Degree
- Experience making/updating Finite Element Models (FEM) in Patran, Hypermesh, FEMAP, or similar
- Experience with running and interpreting Modal Analysis (SOL103), Random Vibration (SOL111), Transient Analysis (SOL112), Nonlinear analysis (SOL106/400)
- Experience with developing vibration environments for aircraft (Mission Based Analysis) and maintaining Environment Criteria Documents (ECD)
- Experience with vibroacoustic and data processing
- Subsystem qualification experience (vendor testing, interpreting previous qualification data and making assessment to current predicted environments, delta qual, etc.)
- Proficient in scripting language (MatLab, Python, VBA, C++, etc.)
- Experience with documenting technical results and analysis and presenting to customers in an effective wayDesired skills :
- Proficient in MSC/Hexagon ADAMs for mechanism and landing gear
- Familiar with RCC31
- Experience with structural analysis for preliminary sizingRequired skills: Bachelors degree in an engineering technical discipline such as Mechanical, Aerospace, or Aeronautical; 9 years experience with a Bachelors Degree or 7 years with a Masters DegreeExperience making/updating Finite Element Models (FEM) in Patran, Hypermesh, FEMAP, or similarPrevious experience in a scripting language (MatLab, Python, VBA, C++, etc.)
- STD 810Experience with vibroacoustic and data processingSubsystem qualification experience (vendor testing, interpreting previous qualification data and making assessment to current predicted environments, delta qual, etc.)
Airframe Structures Dynamics Engineer - Palmdale, United States - Butler Aerospace and Defense
Description
Airframe Structures Dynamics EngineerLocation:
Palmdale, CAJob ID: #69136
Pay Range:
$100-120Seeking a full-time Airframe Structures Dynamics Engineer for the Advanced Development Programs (ADP) in Palmdale, California. A successful candidate will apply technical expertise in developing solutions to aircraft structural design problems.
Responsibilities for this position may include:
Basic Qualifications :
(SOL103), Random Vibration (SOL111), Transient Analysis (SOL112), Non-linear analysis (SOL106/400)
Experience with developing vibration environments for aircraft (Mission Based Analysis) and maintaining Environment Criteria Documents (ECD) of MIL
We recognize that we thrive on diversity and inclusion for the benefit of our employees, our customers, and the communities where we are located.
Employment decisions are made without regard to race, color, religion, gender, national origin, ethnicity, veteran status, disability status, age, sexual orientation, gender identity, gender expression, marital status, mental or physical disability or any other legally protected status.
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