Efficient Nonlinear Dynamic Analyses of Aircraft Structural Components With Various Boundary Conditions Using the Koiter-Newton Model Reduction
AIAA SCITECH 2025 Forum
01.01.2025
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Buckling Imperfection-Sensitivity Analysis Using a Koiter-Newton Approach
British Library Conference Proceedings | 2013
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