Stress – Static Composite, Fuselage

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 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...

Overview: 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) Well versed in ISAMI...

Overview: Static -Fuselage - 1 Opening **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...

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...

Overview: 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 - Experience in...

Overview: Stress engineer Statics - 2- 3 Years **Responsibilities**: Knowledge of aircraft loads Experienced in spectrum generation, - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section) - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wing section, Flaps, Carriages) - Well versed...

Overview: Stress engineer Statics - 5- 6 Years **Responsibilities**: Knowledge of aircraft loads Experienced in spectrum generation, - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section) - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wing section, Flaps, Carriages) - Well versed...

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 ...

Overview: - Extensive Knowledge of aircraft structure and aircraft loads - Experience on non-Airbus 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) -...

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...

Versatile experience on Analysis of Primary & Secondary (Fuselage, Wing and Empennage) structures - Good working experience in MRB / Concession on Metallic and Composite primary and Secondary structures - Airbus project exp is must - Very Strong knowledge on Strength of Materials and Engineering Mechanics - Expertise in Static and Fatigue and Damage...

Overview: F&DT- Fuselage - 1 Opening **Responsibilities**: - Knowledge of aircraft loads - Experienced in spectrum generation and Kt Calculation - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section) - Well versed in ISAMI modules (including crack models, joint models)and ISAMI template preparation - Sizing and...

Responsibilities • Knowledge of aircraft loads  • Experienced in spectrum generation and Kt Calculation • Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section)  • Well versed in ISAMI modules (including crack models, joint models)and ISAMI template preparation  • Sizing and stress analysis of the...

About UsAXISCADES is a technology solutions company focusing on engineering solutions and services. We bring expertise that caters to the engineering, technology, manufacturing and digital needs of fortune 100 clients in aerospace, defense, heavy engineering, automotive, energy & medical equipment sectors. With decades of experience in creating innovative,...

About UsAXISCADES is a technology solutions company focusing on engineering solutions and services. We bring expertise that caters to the engineering, technology, manufacturing and digital needs of fortune 100 clients in aerospace, defense, heavy engineering, automotive, energy & medical equipment sectors. With decades of experience in creating innovative,...

Responsibilities • Working experience on the E2E or Design concession Assessment/ Validation for Aircraft Fuselage/wing components concessions for metallic/composite • Hands-on execution of Aerostructures composite/Metallic Fuselage /Wing concessions. • Good knowledge on Airbus Assembly and Shopfloor knowledge • Perform all the above activities...

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

Expertise in Fatigue and Damage tolerance of metallic structures using FEA and hand calculation - Good working experience of metallic primary and secondary structures. - Expertise in analyzing airframe structures - Expertise in Engineering mechanics and analytical calculation using classical methods - Stress/Load FEM extraction from GFEM/DFEM - Expertise in...