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Title:

Aeroelastic Analysis of a Flutter Demonstrator with a Very Flexible High-Aspect-Ratio Swept Wing

Document type:
Konferenzbeitrag
Contribution type:
Textbeitrag / Aufsatz
Author(s):
Rozov, V.; Hermanutz, A.; Breitsamter, C.; Hornung, M.
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 high-...     »
Keywords:
flutter; small-disturbance CFD; structural dynamics; aeroelasticity; flexible wing
Dewey Decimal Classification:
620 Ingenieurwissenschaften
Book / Congress title:
IFASD [International Forum on Aeroelasticity and Structural Dynamics]
Date of congress:
25.-28.6.
Year:
2017
Pages:
13 S.
Reviewed:
ja
Language:
en
TUM Institution:
Lehrstuhl für Leichtbau
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