Sathish Lakshmana

Airbus A350 Freighter - MDCD & Door Surround Structures •Conduct crippling, inter-rivet buckling, and freeflange stability assessments. •Perform static sizing and detailed evaluation for metallic & composite components. •Deliver comprehensive stress reports aligned with Airbus certification standards.

Project 1: Static Strength Analysis - A320neo XLR & Single Aisle (Inboard Wing Ribs) •Performed static strength evaluations including pulloff, crushing, and combined loading. •Analyzed load redistribution effects (mouse holes, castellations). •Defined panel properties, equivalent thickness, and stiffness. •Interpreted ISAMI results and produced certification dossiers. Project 2: FE Modelling - Wing Primary Structures •Built high-fidelity FE models ensuring structural realism and correct load paths

Bombardier Global 7000 Program •Conducted static, buckling, crippling, and fastener analysis for secondary structures. •Executed load transfer, section strength checks, and classical hand calculations.

A350-900/ 1000 Cutouts, Corner Fittings & System Hole Sizing •Meshed primary/ secondary structures; updated materials per MSN. •Performed GFEM-DFEM condensation, integration, and validation. •Conducted ISAMI DT & strength analyses (notch, filled hole CFRP/ metallic). •Executed SOL101/ 103/ 105 analysis for critical load cases. •Delivered AM2036 and FFC certification-ready reports. Upper Shell Brackets - Static Strength Analysis •Evaluated stresses, fastener loads, and reserve factors.