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Design of kinematic mechanism of morphing wing with functionally gradient metamaterial skin

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F26%3A0199148" target="_blank" >RIV/00216305:26210/26:0199148 - isvavai.cz</a>

  • Result on the web

    <a href="http://dx.doi.org/10.1201/9781003677895-155" target="_blank" >http://dx.doi.org/10.1201/9781003677895-155</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1201/9781003677895-155" target="_blank" >10.1201/9781003677895-155</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Design of kinematic mechanism of morphing wing with functionally gradient metamaterial skin

  • Original language description

    Morphing aircraft wings provide a nature-inspired solution to reduce air drag for different phases of flight, thereby reducing overall fuel consumption and environmental impact. A wing leading edge composed of a flexible metamaterial skin and a rigid kinematic mechanism that changes the skin profile into target shapes is proposed. The design process consists of two parts – A) the finding of the geometric parameters of the skin with gradient bending stiffness, and B) the synthesis of the kinematic mechanism. The metamaterial skin is represented by a simplified spring model describing significant mechanical properties of the structure. The advantage of this approach is the significantly reduced computational time to simulate this complex metamaterial geometry compared to the use of other modeling methods such as FEM. A differential evolution (DE) algorithm is used to optimize the geometric parameters of the skin to find a suitable combination of the geometric parameters of the structure to minimize deviation of the achieved deformed shape of the skin from the target shapes. At the same time, the effect of aerodynamic loads is already included at this stage of the skin design as beneficial forces helping with the skin deformation. The rigid morphing mechanism is designed using vector method based on the optimized positions of attachment points. A demonstrator is fabricated using 3D printing based on the optimized geometry of the skin and morphing mechanism.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20300 - Mechanical engineering

Result continuities

  • Project

  • Continuities

    R - Projekt Ramcoveho programu EK

Others

  • Publication year

    2025

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    Engineering Materials, Structures, Systems and Methods for a More Sustainable Future

  • ISBN

    9781003677895

  • ISSN

  • e-ISSN

  • Number of pages

    6

  • Pages from-to

    928-933

  • Publisher name

    CRC Press

  • Place of publication

    London

  • Event location

    Cape Town

  • Event date

    Sep 1, 2025

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article