Stress – FEM, EUK

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: 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: 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: - 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) -...

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...

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...

Overview: Good Knowledge on Aerospace domain, structure, loads & Aircraft drawing Experience on the Stress Assessment for Aircraft wing components concessions. In depth knowledge of stress, fatigue and damage tolerance analysis of metallic structures (Fatigue analysis as per M2841) Effect of non-conformities of metallic and composite structures (good...

Overview: - Knowledge of aircraft and understanding the functions of various aerospace components - Expert in Finite element meshing (1D, 2D, 3D ) using Hypermesh - DFEM & GFEM - 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 modifying the...

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...

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 •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) • 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...

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...

**Job Description**: - 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...

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 ...

Quest Global is an organization at the forefront of innovation and one of the world’s fastest growing engineering services firms with deep domain knowledge and recognized expertise in the top OEMs across seven industries. We are a twenty-five-year-old company on a journey to becoming a centenary one, driven by aspiration, hunger and humility. We are...

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...

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: 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...