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Dokumenttyp:
Konferenzbeitrag 
Art des Konferenzbeitrags:
Textbeitrag / Aufsatz 
Autor(en):
Rozov, V.; Hermanutz, A.; Breitsamter, C.; Hornung, M. 
Titel:
Aeroelastic Analysis of a Flutter Demonstrator with a Very Flexible High-Aspect-Ratio Swept Wing 
Abstract:
The goal to develop aircraft which are greener, safer, and more cost effective can be only maintained by significant innovations in aircraft design methods. An integrated mul- tidisciplinary design approach can lead to a considerable performance enhancement of future derivative aircraft. Advanced aerodynamic and structural design technologies can be achieved by passive as well as active suppression of aeroelastic instabilities. To demonstrate the potential of this approach, an UAV with a hig...    »
 
Stichworte:
flutter; small-disturbance CFD; structural dynamics; aeroelasticity; flexible wing 
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften 
Kongress- / Buchtitel:
IFASD [International Forum on Aeroelasticity and Structural Dynamics] 
Konferenzort:
Como, Italy 
Datum der Konferenz:
25.-28.6. 
Jahr:
2017 
Seiten:
13 S. 
Reviewed:
ja 
Sprache:
en 
TUM Einrichtung:
Lehrstuhl für Leichtbau