Ph3Your mission /h3 pbKey Tasks /b /p ul liPerform structural and aerodynamic load analysis. /li liDevelop, validate and maintain dynamic and aeroelastic models using CAMRAD II, FLIGHTLAB, Simulink, and NASTRAN. /li liSupport structural test campaigns including static and dynamic testing, modal analysis, and Ground Vibration Testing (GVT). /li liAnalyze vibration phenomena and contribute to the design and tuning of dampers and passive/active mitigation solutions. /li liEvaluate system stability in both low- and high-frequency domains. /li liEnsure compliance with relevant aerospace standards (e.g., DO-160, MIL-STD-810, MIL-A-8866). /li liSupport flight and ground test activities, including instrumentation definition and data analysis. /li liInterface with control systems engineers to integrate loads and dynamics considerations into flight control strategy. /li liPrepare technical documentation, presentations, and reports for internal use and qualification purposes. /li /ul h3Your profile /h3 pbQualifications /b /p ul liMSc or PhD in Aerospace Engineering or related field, with a specialization in flight dynamics, structural dynamics, or aeroelasticity. /li liHands‑on experience with structural testing (static and dynamic), GVT, and vibration analysis. /li liProficiency with engineering software such as MATLAB, Simulink, FLIGHTLAB, CAMRAD II, and NASTRAN. /li liStrong understanding of helicopter aeromechanics, aeroelastic phenomena, and structural loads methodology. /li liFamiliarity with aerospace certification standards including DO-160 and relevant MIL-STD documents. /li liExperience in analyzing damping strategies and system stability for rotorcrafts. /li liStrong communication skills and ability to work collaboratively across disciplines. /li liFluent in English (written and spoken). German desirable. /li libEligibility: /b Swiss or EU citizens only. /li libLocation: /b On‑site in Näfels | Bilten, Switzerland. /li /ul /p #J-18808-Ljbffr