Aeroelasticity & Structural Dynamics.

Descripción de la oferta

Aeroelasticity & Structural Dynamics.

Airbus Defence & Space Getafe (ex Airbus Military)

Airbus Defence and Space is a division of Airbus Group formed by combining the business activities of Cassidian, Astrium and Airbus Military. The new division is Europe's number one defence and space enterprise, the second largest space business worldwide and among the top ten global defence enterprises. It employs some 40,000 employees generating revenues of approximately €14 billion per year.

Airbus is a global leader in aeronautics, space and related services. In 2016, it generated revenues of € 67 billion and employed a workforce of around 134,000. Airbus offers the most comprehensive range of passenger airliners from 100 to more than 600 seats. Airbus is also a European leader providing tanker, combat, transport and mission aircraft, as well as Europe's number one space enterprise and the world's second largest space business. In helicopters, Airbus provides the most efficient civil and military rotorcraft solutions worldwide.

Our people work with passion and determination to make the world a more connected, safer and smarter place. Taking pride in our work, we draw on each other's expertise and experience to achieve excellence. Our diversity and teamwork culture propel us to accomplish the extraordinary - on the ground, in the sky and in space.

Description of the job

A vacancy for a Aeroelasticity & Structural Dynamicshas arisen within Airbus Defence & Space Getafe (ex Airbus Military).The successful applicant will join TAEGD department.

Perfil buscado

Tasks & accountabilities

The main tasks are:

·  Full aircraft dynamic modeling using Finite Element Method (FEM) Technique. Normal modes analysis. Update FE model to match Ground Vibration Test (GVT) results.
·  Unsteady aerodynamics modeling. Doublet Lattice Method (DLM). Update model to match CFD, Wind Tunnel Test, Flight Test.
·  Static aeroelastic analysis of components and full aircraft including divergence and control reversal analysis.
·  Flutter analysis. Normal cases. Failure cases. EFCS failure cases. Limit Cycle Oscillations (LCO).
·  GVT specification. GVT performance using LMS software. Experimental modal Analysis results.
·  Flight Flutter Test (FVT) specification. FVT performance using jFlutter tool. FVT results.
·  Update aeroelastic models to match FVT
·  Ground Dynamic loads analysis (Dynamic Landing, Taxi, Nose Wheel Imbalance (NWI), etc.
·  Flight Dynamic Loads (Discrete Tuned Gust (DTG), Continuous Turbulence (CT), Buffet, Blade Loss, Wind milling, etc.)
·  Impacts analysis (bird strike, ice impacts, tyre debris, crashworthiness, ditching, wheels up landing, etc.)

Required skills

We are looking for candidates with the following skills and experience:

·  Advanced level in English.
·  Advanced level in Spanish.
·  German or French would be an asset.
·  Strong interpersonal and communication skills.
·  Able to propose new ideas.
·  Able to work in a multi-cultural environment.