Stress Engineer FDT Wing

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...

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: 2 – 10 YearsKnowledge of aircraft loads Experienced in spectrum generation and Kt Calculation Good in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (wingsection)Well versed in ISAMI modules (including crack models, joint models)and ISAMI template preparationSizing and stress analysis of the Wing...

Overview: - Knowledge of aircraft and understanding the functions of various aerospace wing components - Expert in Finite element modeling using Hypermesh (1D, 2D, 3D ) and 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 submitting and...

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...

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...

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...

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...

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...

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...

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...

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: 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...

JobDescription: Experience:2 – 10 YearsKnowledgeof aircraftloadsExperiencedin spectrum generation and KtCalculationGoodin Fatigue and Damage Tolerance (F&DT) calculations ofAirbus aircrafts (fuselage section)Well versed in ISAMI modules (including crack models jointmodels)and ISAMI template preparationSizingand stress analysis of the Fuselage Structure...

JobDescription: Experience:2 – 10 YearsKnowledgeof aircraftloadsExperiencedin spectrum generation and KtCalculationGoodin Fatigue and Damage Tolerance (F&DT) calculations ofAirbus aircrafts (fuselage section)Well versed in ISAMI modules (including crack models jointmodels)and ISAMI template preparationSizingand stress analysis of the Fuselage Structure...

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: 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...

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...

ResponsibilitiesGood Knowledge on Aerospace domain, Primary and Secondary Structures, loads & Aircraft drawingHands-on execution of Aero-structure Metallic and Composite concessions (Aircraft fuselage, Pylon and Wing components)In depth knowledge of stress, fatigue and damage tolerance analysis of metallic structures (Fatigue analysis as per M2841).In depth...

Applicants can submit CV direct to Email : Syamala Kurumaddali; >Experience : 5 - 15 YearsAbout the company:Quest Global is an organization at the forefront of innovation and one of the worlds fastest growing engineering services firms with deep domain knowledge and recognized expertise in the top OEMs across seven industries. We are a twenty-five-year-old...