Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Design and manufacturing of conformal ablative heatshields
Rapid determination of mass and stiffness distribution on primary skin-stiffener structures
Multi-physics high resolution topology optimization for aerospace structures
Aeroelastic design of a lightweight distributed electric propulsion aircraft with flutter and strength requirements
Adjoint-based aeroelastic optimization with high-fidelity time-accurate analysis