Stress - Fem, Static, Wing - Euk

**Overview**: F& DT - EUK **Responsibilities**: "- Knowledge of aircraft loads - Experienced in spectrum generation, - Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wing section) - Well versed in ISAMI modules and ISAMI template preparation - Sizing and stress analysis of the wing Structure and interfaces by means of hand...

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...

Role: Stress - Static Composite, Wing Full Time Location - Bangalore (Hybrid) Exp - 8 - 10 Years JOB DESCRIPTION: - 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...

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...

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...

JobDescription: Experience: 5– 10 YearsKnowledgeof aircraft Fuselage structure and aircraftloadsExperiencedin the static calculations of Airbus aircrafts (wing section)Sizingand stress analysis of the fuselage Structure and interfaces bymeans of hand calculations numerical simulations(FEM)Well versed in ISAMI staticmodules and ISAMI template...

Overview: Stress - Static Composite **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...

Overview: Structural stress Engineer - Static & FD&T **Responsibilities**: Static: Knowledge of aircraft loads Experienced in the static calculations of Airbus wing structures such as Flaps, slats, carriages etc Experience in numerical modeling, post-processing and reporting of the results Good understanding of load transfer between various high lift...

Job Description: -Experience: 8 – 10 Years Knowledge of aircraft Fuselage structure and aircraft loadsExperienced 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...

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...

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...

**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...

**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...

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) -...

ResponsibilitiesKnowledge 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 (FEM)•...

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...

JobDescription: Experience:2 – 10 Years Knowledgeof aircraft loadsExperiencedin spectrum generation and KtCalculationGoodin Fatigue and Damage Tolerance (F&DT) calculations ofAirbus aircrafts (wing section)Wellversed in ISAMI modules (including crack models joint models)andISAMI template preparation Sizingand stress analysis of the Wing Structure and...

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 ...