Stress Static Checker

Overview: Extensive Knowledge of aircraft structure and aircraft loads Experience on nonAirbus programs with a broad knowledge of hand calculations and not be FEM reliant Expert in the static calculations for sizing and stress analysis of the aircraft structures, interfaces by means of hand calculations, valid methods, numerical simulations (FEM) Understand...

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...

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...

ResponsibilitiesKnowledge of aircraft structure and aircraft loads• Experience on non-Airbus programs with a broad knowledge of hand calculations and not be FEM reliant• Experienced in the static calculations for sizing and stress analysis of the aircraft structures, interfaces by means of hand calculations, valid methods, numerical simulations (FEM)•...

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 ...

Role: Stress - Static Composite, Wing Full Time Location - Bangalore (Hybrid) Exp - 8 - 10 Years JOB DESCRIPTION: - 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...

Responsibilities Knowledge of aircraft structure and aircraft loads • Experience on non-Airbus programs with a broad knowledge of hand calculations and not be FEM reliant • Experienced in the static calculations for sizing and stress analysis of the aircraft structures, interfaces by means of hand calculations, valid methods, numerical simulations...

Responsibilities Knowledge of aircraft structure and aircraft loads • Experience on non-Airbus programs with a broad knowledge of hand calculations and not be FEM reliant • Experienced in the static calculations for sizing and stress analysis of the aircraft structures, interfaces by means of hand calculations, valid methods, numerical simulations...

Responsibilities Knowledge of aircraft structure and aircraft loads • Experience on non-Airbus programs with a broad knowledge of hand calculations and not be FEM reliant • Experienced in the static calculations for sizing and stress analysis of the aircraft structures, interfaces by means of hand calculations, valid methods, numerical simulations...

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...

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...

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...

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...

**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 -...

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 : 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 ...

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 preparation...