Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Allocating Section Thickness and Camber for Transonic Wing Design (AIAA 2014-0024)



    Kongress:

    52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD



    Erscheinungsdatum :

    01.01.2014


    Format / Umfang :

    25 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    A Method to Allocate Camber, Thickness and Incidence on a Swept Wing (AIAA 2014-3172)

    Takahashi, T. / Dulin, D. / Kady, C. et al. | British Library Conference Proceedings | 2014


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

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


    WING SECTION THICKNESS AND CAMBER ALLOCATION FOR CONCEPTUAL AND PRELIMINARY AIRCRAFT DESIGN

    Shajanian, A. / Takahashi, T. / German, B. et al. | British Library Conference Proceedings | 2011


    Wing Section Thickness and Camber Allocation for Conceptual and Preliminary Aircraft Design

    Shajanian, Arvin / Takahashi, Timothy / German, Brian et al. | AIAA | 2011


    Development and Wind Tunnel Test of Variable Camber Morphing Wing (AIAA 2014-1261)

    Yokozeki, T. / Sugiura, A. / Hirano, Y. et al. | British Library Conference Proceedings | 2014