Static Analysis || Airbus

Job Description: Stress analysis of metallic and composite aircraft structures using hand calculations, ISAMI, GFEM and DFEMs Extraction of loads, stresses, generation of spectra and mission files Extraction of material data, geometry details and fastener specifications from part & amp; assembly drawings Application of appropriate static, fatigue and...

Job Description: Stress analysis of metallic and composite aircraft structures using hand calculations, ISAMI, GFEM and DFEMs Extraction of loads, stresses, generation of spectra and mission files Extraction of material data, geometry details and fastener specifications from part & amp; assembly drawings Application of appropriate static, fatigue and...

Job Description: Get comprehensive understanding of Airbus best practices, methods, processes, tools and framework in Structural Analysis domain, with a specific focus on Nonlinear Static and Dynamic (Crash/Impact) finite element analysis and assessing the mechanical behaviour of metallic and composite structures Perform FEA (finite element analysis)...

Job Description: Analyze and Validate metallic structures for static & fatigue strength according to validated methods. Ensure adherence to regulations, relevant design principles, processes, methods and manufacturing capabilities guidelines. Define, interpret and validate tests. Interface and communicate with relevant stakeholders. Provide relevant input...

Job Description: Knowledge Fatigue and Damage Tolerance analysis Theoretical knowledge in aircraft crack propogation analysis Knowledge of aircraft loads and experienced in spectrum generation  Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases. ...

Job Description: Knowledge Fatigue and Damage Tolerance analysis Theoretical knowledge in aircraft crack propogation analysis Knowledge of aircraft loads and experienced in spectrum generation  Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases. ...

Job Description: Internship – 4 - 6 MonthsAI (Artificial Intelligence) for Autonomous Aviation-TechnologyAirbus IP Analytics and Intelligence is an integral part of the Airbus Intellectual Property Departmentand is based out of Bangalore, India. IP analytics team is to provide technical intelligence based onpublicly available patent data combined with...

Job Description: -  Experience: 8 – 10 Years Knowledge of aircraft Fuselage structure and aircraft loads  Experienced in the static calculations of Airbus aircrafts (wing section)  Knowledge and experience on composites and sandwich structuresSizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical...

Job Description: -  Experience: 8 – 10 Years Knowledge of aircraft Fuselage structure and aircraft loads  Experienced in the static calculations of Airbus aircrafts (wing section)  Knowledge and experience on composites and sandwich structuresSizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical...

Job Description: About Organization: As a proven leader in the global aerospace sector, Airbus designs, produces and delivers innovative solutions with the aim to create a better-connected, safer and more prosperous world. A commercial aircraft manufacturer, with Space and Defense as well as Helicopters Divisions, Airbus is the largest aeronautics and...

Job Description: About Organization: As a proven leader in the global aerospace sector, Airbus designs, produces and delivers innovative solutions with the aim to create a better-connected, safer and more prosperous world. A commercial aircraft manufacturer, with Space and Defense as well as Helicopters Divisions, Airbus is the largest aeronautics and...

Job Description: -  Experience: 5 – 10 Years Knowledge of aircraft Fuselage structure and aircraft loadsExperienced in the static calculations of Airbus aircrafts (wing section)  Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM) Well versed in ISAMI static modules and ISAMI...

Job Description: -  Experience: 5 – 10 Years Knowledge of aircraft Fuselage structure and aircraft loadsExperienced in the static calculations of Airbus aircrafts (wing section)  Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM) Well versed in ISAMI static modules and ISAMI...

Responsibilities Knowledge of aircraft Fuselage structure and aircraft load Experienced in the static calculations of Airbus aircrafts (wing section) Knowledge and experience on composites and sandwich structures Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM) ...

Job Description: This position will be responsible for performing technical analysis for in-service incidents reported by operators to Airbus customer services, product safety and acceptance flights by decoding the flight recorder data, analyzing the reported incident and providing internal customers with validated information in due time and appropriate...

Job Description: This position will be responsible for performing technical analysis for in-service incidents reported by operators to Airbus customer services, product safety and acceptance flights by decoding the flight recorder data, analyzing the reported incident and providing internal customers with validated information in due time and appropriate...

Job Description : Static Analysis with Airbus Methods and Procedures. Minimum of 4 years execution experience on any of the two main Aircraft Primary structures (NCF, Center Fuselage, Empenage,Wing upper cover, VTP, HTP, Door Surrounds, Doors, Pylon) Minimum of 1 year execution experience on MSI, ESI, Hydraulic Brackets static stress analysis...

Job Description : Static Analysis with Airbus Methods and Procedures. Minimum of 4 years execution experience on any of the two main Aircraft Primary structures (NCF, Center Fuselage, Empenage,Wing upper cover, VTP, HTP, Door Surrounds, Doors, Pylon) Minimum of 1 year execution experience on MSI, ESI, Hydraulic Brackets static stress analysis...

Responsibilities •Knowledge of aircraft Fuselage structure and aircraft loads• Experienced in the static calculations of Airbus aircrafts (fuselage section)• Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM)• Well versed in ISAMI static modules and ISAMI template...

Responsibilities •Knowledge of aircraft Fuselage structure and aircraft loads• Experienced in the static calculations of Airbus aircrafts (fuselage section)• Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM)• Well versed in ISAMI static modules and ISAMI template...