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Title:

AERODYNAMIC ANALYSIS OF A FULL MODEL WITH ADAPTIVE ELASTO-FLEXIBLE MEMBRANE WINGS

Document type:
Konferenzbeitrag
Contribution type:
Textbeitrag / Aufsatz
Author(s):
Pflueger J.; Hirschmann K.; Breitsamter C.
Abstract:
Unmanned and micro aerial vehicles operate under a variety of flight conditions. The application of morphing wings for these aircraft offer the possibility to adapt the aerodynamics to different flight stages. The investigated model consists of two deformable wing structures, which are covered by an elastic membrane. The concept enables wing folding over a wide range and it allows the wing to adapt to changing aerodynamic loads. The present study focuses on the fluid-structure-interaction simula...     »
Keywords:
Flexible wing surface; Fluid-structure-interaction simulation; Morphing camber; Morphing wing
Dewey Decimal Classification:
620 Ingenieurwissenschaften
Book / Congress title:
International Council of the Aeronautical Sciences
Congress (additional information):
32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021, Shanghai, 6 September 2021 through 10 September 2021, Code 176566
Year:
2022
Covered by:
Scopus
Print-ISBN:
978-393218291-4
Language:
en
TUM Institution:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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