.png){kind=icon}
.png){kind=icon}
Return
Modified Craig-Bampton Method Based on Static Correction Procedure
.png){kind=icon}
PRE
AI
DOI：10.2514/1.J066399.png)
.png){kind=icon}
Original request for help.png){kind=icon}
Share.png){kind=icon}
Save
Abstract
En
Keywords:
Reduced Order Modelling
Structural Finite Elements
Aircraft Wing Design
Turbine Blades
Model reduction
Guyan method
Craig-Bampton method
Static correction procedure
High-order fixed-interface modes