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Analyze turbomachinery performance and design compressor/turbine stages for propulsion systems
Evaluate avionics designs against DO-178C/DO-254 standards and generate certification documentation
Analyze composite laminates and predict failure modes using Classical Lamination Theory
Synthesize avionics requirements, FMEA, and DO-178C compliance matrices
Systematically interpret CFD results and validate aerodynamic coefficients against experimental data
Rapid fatigue life prediction and damage tolerance analysis for aerospace structures
Systematically diagnose avionics failures with compliance-ready root cause analysis
Analyze turbomachinery performance with thermodynamic calculations and diagnostics
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