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Titel:

High Fidelity Trim Calculation Under Consideration Of Aeroelastic Effects Of A High Aspect Ratio Swept Wing

Dokumenttyp:
Konferenzbeitrag
Art des Konferenzbeitrags:
Textbeitrag / Aufsatz
Autor(en):
Hermanutz, A.; Hornung, M.
Abstract:
New structural wing technologies like morphing structures, high aspect ratio wings or passive as well as active load elevation techniques have in common that flexibility is increasing within the next generation of aircraft wings. Therefore, the aeroelastic effects will rise and sophisticated methods are needed to develop and predict the aircrafts properties, load and overall behavior on a highly accurate level. The presented paper shows the work on virtual aircraft models and the application of...     »
Stichworte:
Computational Fluid Structure Interaction; High Aspect Ratio Wings; Structural Wing Design
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
IFASD [International Forum on Aeroelasticity and Structural Dynamics]
Datum der Konferenz:
25.-28.6.
Jahr:
2017
Seiten:
16 S.
Reviewed:
ja
Sprache:
en
TUM Einrichtung:
Lehrstuhl für Leichtbau
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