Stress - Static Composite, Wing - Euk

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 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...

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 ...

Overview:Good Knowledge on Aerospace domain, structure, loads & Aircraft drawingExperience 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...

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 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: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...

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...

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...

We are looking for a skilled professional to join our team:Experience: 2 – 10 YearsKnowledge of aircraft loadsExperienced in spectrum generation and Kt CalculationGood in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wing section)Well versed in ISAMI modules (including crack models joint models) and ISAMI template preparationSizing...

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...

Static Analysis with Airbus Methods and Procedures Minimum of 4 6 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 Hands on execution experience on GFEM Load extraction DFEM Creation Validation and Post processing F DT Hands on execution experience...

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...

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...

Job Description:Experience: 2 – 10 Years Knowledge of aircraft loads Experienced in spectrum generation and Kt Calculation Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wing section) Well versed in ISAMI modules (including crack models, joint models)and ISAMI template preparation Sizing and stress analysis of the Wing...

Responsibilities 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...

Overview:Static -Fuselage - 3 OpeningResponsibilities: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...