Engineer - Aircraft Component Analysis - Static

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...

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:Knowledge Fatigue and Damage Tolerance analysisTheoretical knowledge in aircraft crack propogation analysisKnowledge of aircraft loads and experienced in spectrum generationCalculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases.Calculation...

Job Description: Knowledge Fatigue and Damage Tolerance analysisTheoretical knowledge in aircraft crack propogation analysisKnowledge of aircraft loads and experienced in spectrum generation Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS...

Short DescriptionCreation/Modification of GFEM/DFEM for metallic/composite primary and secondary structuresCreation/Modification of ISAMI files for aerostructures sizingDevelopment of Analytical/Hand Calculations for Joints, lugs and SectionsCreation/Modification of Stress SheetsCreation/Modification of Stress Certification ReportsPlanning and Interface with...

**Short Description**: - **Creation/Modification of **GFEM/DFEM for metallic/composite primary and secondary structures**: - **Creation/Modification of **ISAMI files for aerostructures sizing**: - **Development of Analytical/ **Hand Calculations for Joints, lugs and Sections**: - **Creation/Modification of Stress Sheets**: - **Creation/Modification of...

Short Description Creation/Modification of GFEM/DFEM for metallic/composite primary and secondary structures Creation/Modification of ISAMI files for aerostructures sizing Development of Analytical/Hand Calculations for Joints, lugs and Sections Creation/Modification of Stress Sheets Creation/Modification of Stress Certification Reports ...

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...

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)•...

Overview: Static -Fuselage - 3 Opening **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...

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,...

Short DescriptionCreation/Modification of GFEM/DFEM for metallic/composite primary and secondary structuresCreation/Modification of ISAMI files for aerostructures sizingDevelopment of Analytical/Hand Calculations for Joints, lugs and SectionsCreation/Modification of Stress SheetsCreation/Modification of Stress Certification ReportsPlanning and Interface with...

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...

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...

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...

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: -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 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...

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...