In this paper, design criteria are proposed for an aircraft morphing wing skin and conventional lattice structures are evaluated against the design criteria. Although the structural deformation and aerodynamic loadings during the morphing process directly affect the skin structure, the design of the morphing skin has been overlooked. Five design criteria for the morphing skin of a variable camber compliant wing were derived from structural analysis results and reference values. According to the evaluation of conventional lattice structures, it is concluded that there is an absolute need for a new structure that satisfies the required design criteria.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Design Criteria for Variable Camber Compliant Wing Aircraft Morphing Wing Skin


    Beteiligte:
    You, Hangil (Autor:in) / Kim, Seongik (Autor:in) / Yun, Gun Jin (Autor:in)

    Erschienen in:

    AIAA Journal ; 58 , 2 ; 867-878


    Erscheinungsdatum :

    01.02.2020




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Variable Camber Compliant Wing - Design

    Joo, James J. / Marks, Christopher R. / Zientarski, Lauren et al. | AIAA | 2015


    Variable camber adaptive compliant wing system

    JOO JAMES J | Europäisches Patentamt | 2016

    Freier Zugriff

    Variable camber adaptive compliant wing system

    JOO JAMES J | Europäisches Patentamt | 2018

    Freier Zugriff

    Variable Camber Compliant Wing - Design (AIAA 2015-1050)

    Joo, James J. / Marks, Christopher R. / Zientarski, Lauren et al. | British Library Conference Proceedings | 2015


    Variable Camber Compliant Wing - Wind Tunnel Testing

    Marks, Christopher R. / Zientarski, Lauren / Culler, Adam J. et al. | AIAA | 2015