Stress Engineer Static Composite

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...

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...

Responsibilities 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) ...

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...

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...

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...

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...

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...

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 Location: Bangalore/ Chennai/ Pune/ Coimbatore Experience -5-15 years Roles: 1) Stress - F&DT 2) Stress - Static Metallic 3) Stress - Static Composite 4) Stress - FEM 5) Stress- Hypermesh Essential Skills: Airbus (A320/ A350/ A380, etc) ISAMI Hyper view (Postprocessing knowledge) Catia V5, ZAMIZ/AIRENA(Basic knowledge) Excel & VBA ...

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: Should have Strong knowledge and experience in Aerospace Industry and expertise in Structural analysis ( Both Static and Fatigue) Hands-on Experience on Aircraft Nacelle components is preferrable. Should be well-versed with Classical and Finite element analysis approaches. Should able to review and validate the results for both Metallic...

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...

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...

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

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