User: Guest  Login
Title:

Virtual Aaircraft Model for Aeroelastic Simulation and Load Prediction of a High-Aspect Ratio Composite Swept Wing

Document type:
Konferenzbeitrag
Author(s):
Andreas Hermanutz, Mirko Hornung
Abstract:
An approach for a virtual aircraft model with the purpose to simulate the static and dynamic aeroelastic behavior of a flexible aircraft is presented. To reduce the computational effort, methods for accurate model reduction and their applicability for a flexible aircraft configuration is investigated. Static and dynamic flight maneuvers are performed to identify critical load conditions, which are furhter used with the inverse transformation for detailed structural sizing. As a computa...     »
Keywords:
Aircraft Aeroelasticity, Model Reduction, High AR-Wing
Book / Congress title:
International Council of the Aeronautical Sciences
Year:
2018
 BibTeX