Stress Engineer; m​/f​/d

Tasks

• Stress analysis of metallic or composite primary and secondary components by means of hand calculations and/or FEM
• Write structural substantiation reports that meet the technical requirements of the program and certifying authority
• Liaise, manage and provide technical direction to offsite suppliers
• Provide stress support to other areas of the organization, including Design, Production, Flight Test, Quality Assurance and Airworthiness
• Ensure that the technical content, quality, compliance and safety aspects of any technical data is documented in accordance with internal standards and guidelines

• Strong knowledge of the fundamental principles of stress analysis of metallic and composite structures
• Good understanding of aircraft structural load paths and experience with analysis methodologies for various primary and secondary structural components
• Capability to set-up an FE model based on DMU or design principles
• Advanced skills with Nastran, Hypermesh and Patran (pre/post processors & solvers)
• Experience with classic hand calculation stress methods (e.g. HSB, Bruhn, ESDU, Roark & Young)
• Capable of working to deadlines and following internal calculation procedures
• Ability to work independently and multitask efficiently
• Understanding of civil aircraft certification rules and experience in certification procedures (ideally JAR/CS/FAR 23)
• Strong motivation and enthusiasm to achieve company goals and objectives
• Ability to work on details while keeping the big picture in mind
• Very good knowledge of spoken and written English;
  German is a plus
• Experience with Fatigue & DT analysis of airframe components is a plus
• Experience using Siemens Teamcenter PLM Software (version 10.x) is a plus
• Master’s degree in aeronautical engineering or equivalent education/experience in the aeronautical industry
• Minimum of 7 years engineering experience in stress analysis