Stress – Static Metallic, Fuselage

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...

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 ...

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...

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...

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...

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...

ResponsibilitiesKnowledge of aircraft loadsExperienced in spectrum generation and Kt CalculationGood 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 preparationSizing and stress analysis of the Fuselage Structure and interfaces by...

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...

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 GFEM/DFEM...

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,...

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...

Role: Stress EngineerWork Location: BangaloreExperience: 2 to 6 yrsMode of job: FulltimeJob Description:Hand calculation knowledge through classical approach using strength of materials and free body concepts.Able to understand the technical requirements and have basic understanding on loads and their behavior.Should be well-versed with Classical analysis...

Role:Stress Engineer Work Location:Bangalore Experience: 2 to 6 yrs Mode of job: Fulltime Job Description: Should have Strong knowledge and experience in Aerospace Industry and expertise in Structural analysis ( Both Static and Fatigue) Carry out hand calculation through classical approach using strength of materials and free body concepts. Hands-on...