Stress – Static Composite, Fuselage

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) ...

JobDescription: Experience: 8– 10Years Knowledgeof aircraft Fuselage structure and aircraft loads Experiencedin the static calculations of Airbus aircrafts (wing section) Knowledgeand experience on composites and sandwichstructures Sizingand stress analysis of the fuselage Structure and interfaces bymeans 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)• 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: -  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...

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...

JobDescription: Experience:2 – 10 Years Knowledgeof aircraftloads Experiencedin spectrum generation and KtCalculation Goodin Fatigue and Damage Tolerance (F&DT) calculations ofAirbus aircrafts (fuselage section) Well versed in ISAMI modules (including crack models jointmodels)and ISAMI template preparation Sizingand stress analysis of the Fuselage...

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: -  Experience: 2 – 10 Years   Knowledge of aircraft loadsExperienced 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...

Job Description: -  Experience: 2 – 10 Years   Knowledge of aircraft loadsExperienced 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...

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...

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 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 ...

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,...