Fuselage / Wing Stress Engineer
1.Perform Static, fatigue and damage tolerance analysis for Aircraft structures using classical hand calculation.
2.Applicant should be familiar with Boeing Static and Book 1,2 and 3 Fatigue Analysis Methodologies
3.Applicant should be familiar with and have prior experience with the following Boeing Stress Tools, including IAS, XSA/SA+, FEADMS, IDTAS, Moss-Duberg, and FAMOSS Understanding of load paths, extraction of loads from Finite Element Models.
4.Applicant should be familiar with Damage Tolerance Analysis and CFR25.571
5.Determination of critical failure modes and performing analysis to ensure structural integrity.
6.Analysis of aircraft primary/secondary metallic structures.
7.Read and interpret engineering drawings.
8.Coordinate with cross functional groups including Design, Materials & Process Engineering.
9.Participate in review meetings with Customer and SMEs.
10.Generate Engineering Stress Report which establishes compliance and safety.
11.Interact with customer; understand the Scope of Work and methodology required to meet customer expectations.
Required Qualifications (Non-negotiable requirements): 1.At least bachelor s degree in mechanical or aerospace engineering 2.At least 5 years (<18years) of experience in Aerospace Industry as a Stress Engineer 3.Comprehensive knowledge Stress analysis of Aero structures.
Preferred Qualifications: 1.Knowledge of Aerospace industry and standards 2.Experience in metallic and Composites structural analysis 3.Experience in Load, stress calculations and preparing technical reports 4.Experience in Finite Element Analysis tools (Nastran, Patran) 5.Experience in static, fatigue and damage tolerance calculations 6.Strong oral and written communication skills 7.Knowledge of Aerospace industry and standards 8.Experienced in PATRAN, NASTRAN, FEMAP 9.Experience in MRB and SRM 10.Experience in CATIA V5, Enovia 11.Strong oral and written communication and interpersonal skills. 12.US National holder/H1B/ EAD/ F1 OPT ( with exp)
1.Perform Static, fatigue and damage tolerance analysis for Aircraft structures using classical hand calculation.
2.Applicant should be familiar with Boeing Static and Book 1,2 and 3 Fatigue Analysis Methodologies
3.Applicant should be familiar with and have prior experience with the following Boeing Stress Tools, including IAS, XSA/SA+, FEADMS, IDTAS, Moss-Duberg, and FAMOSS Understanding of load paths, extraction of loads from Finite Element Models.
4.Applicant should be familiar with Damage Tolerance Analysis and CFR25.571
5.Determination of critical failure modes and performing analysis to ensure structural integrity.
6.Analysis of aircraft primary/secondary metallic structures.
7.Read and interpret engineering drawings.
8.Coordinate with cross functional groups including Design, Materials & Process Engineering.
9.Participate in review meetings with Customer and SMEs.
10.Generate Engineering Stress Report which establishes compliance and safety.
11.Interact with customer; understand the Scope of Work and methodology required to meet customer expectations.
Required Qualifications (Non-negotiable requirements): 1.At least bachelor s degree in mechanical or aerospace engineering 2.At least 5 years (<18years) of experience in Aerospace Industry as a Stress Engineer 3.Comprehensive knowledge Stress analysis of Aero structures.
Preferred Qualifications: 1.Knowledge of Aerospace industry and standards 2.Experience in metallic and Composites structural analysis 3.Experience in Load, stress calculations and preparing technical reports 4.Experience in Finite Element Analysis tools (Nastran, Patran) 5.Experience in static, fatigue and damage tolerance calculations 6.Strong oral and written communication skills 7.Knowledge of Aerospace industry and standards 8.Experienced in PATRAN, NASTRAN, FEMAP 9.Experience in MRB and SRM 10.Experience in CATIA V5, Enovia 11.Strong oral and written communication and interpersonal skills. 12.US National holder/H1B/ EAD/ F1 OPT ( with exp)