Stress - Static Composite, Wing

Overview:Knowledge of aircraft Fuselage structure and aircraft loadExperienced 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 simulations (FEM)Well versed in ISAMI static...

Overview: Stress - Static Composite **Responsibilities**: Knowledge of aircraft Fuselage structure and aircraft load Experienced 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...

Job Description: -Experience: 8 – 10 Years Knowledge of aircraft Fuselage structure and aircraft loadsExperienced 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 simulations...

Position OverviewExperience: 8–10 YearsStrong knowledge of aircraft fuselage structure and aircraft loadsExpertise in the static calculations of Airbus aircraft (wing section)Knowledge and experience on composites and sandwich structuresConduct sizing and stress analysis of the fuselage structure and interfaces through hand calculations and numerical...

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 template...

Job Description:Experience: 5–10 YearsKnowledge 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 template...

JobDescription: Experience: 5– 10 YearsKnowledgeof aircraft Fuselage structure and aircraftloadsExperiencedin the static calculations of Airbus aircrafts (wing section)Sizingand stress analysis of the fuselage Structure and interfaces bymeans of hand calculations numerical simulations(FEM)Well versed in ISAMI staticmodules and ISAMI template...

Overview: - Knowledge of aircraft and understanding the functions of various aerospace wing components - Expert in Finite element modeling using Hypermesh (1D, 2D, 3D ) and should be capable of idealizing the structure both GFEM and DFEM - Experience on using connections like MPCs, Stuck nodes, Glue elements, CFAST etc - Experience in submitting and...

Overview: Stress - Static Composite, Fuselage - EFR **Responsibilities**: - Knowledge of aircraft Fuselage structure and aircraft loads - Experienced in the static calculations of Airbus aircrafts (fuselage section) - Knowledge and experience on composites and sandwich structures - Sizing and stress analysis of the fuselage Structure and interfaces by...

Responsibilities Knowledge of aircraft Fuselage structure and aircraft load Experienced 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 template preparation ...

Responsibilities •Knowledge of aircraft Fuselage structure and aircraft loads • Experienced in the static calculations of Airbus aircrafts (fuselage 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...

**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...

**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 -...

Overview: Structural stress Engineer - Static & FD&T **Responsibilities**: Static: Knowledge of aircraft loads Experienced in the static calculations of Airbus wing structures such as Flaps, slats, carriages etc Experience in numerical modeling, post-processing and reporting of the results Good understanding of load transfer between various high lift...

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 Hands on...

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 simulations...

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 ...

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: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 template...