Project Role : Engineering Services Practitioner
Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management.
Must have skills : Aircraft Structural Analysis
Good to have skills : NA
Minimum 2 year(s) of experience is required
Educational Qualification : Bachelors or Masters degree in Mechanical or Aerospace or Structural engineering
As an Aircraft Structural Analysis Engineer, you will be responsible for providing end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Your typical day will involve working across structural and stress design, qualification, configuration, and technical management.
WHAT’S IN IT FOR YOU?
Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies: Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc.
To support Sizing & Justification phase.
What you would do in this role
Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components.
Experience in Door Surround Structures/Side shells/PAX floors.
Experience in GFEM/DFEM creation and Validation
Knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis.
Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations.
Experience in ISAMI based analysis.
Experience in Buckling and Modal Analysis.
Experience in engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office).
Basic Knowledge on CATIA and experience in reading assembly drawings
Experience in Technical Report writing skills.
Who are we looking for?
1 to 4 years of Aerostructure Stress Analysis Experience
Education: BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject
Ability to work individually.
Supporting continuous improvement initiatives to increase team efficiency.
Highly preferred primary and secondary structure experience with good knowledge of tools and methods.
Hypermesh, Nastran/Patran, ISAMI
Having VBA/Python programming is an added advantage.