The application of well known design concepts with the combined use of thick transonic profiles to aircraft wing design was investigated. Optimization in terms of weight and operational costs was emphasized. It is shown that the usual design criteria and concepts are too restricted and do not sufficiently represent the physical processes over the wing. Suggestions are made for improving this situation, and a design example given. Compared with a wing design according to previously used criteria, the new design is found to be superior in the most important functions. It is concluded that an isobar concept adjusted to the planform in conjunction with an 'organically' designed wing will lead to the weight optimum solutions of wing profiles.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design of a Transonically Profiled Wing


    Beteiligte:
    B. Kiekebusch (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    64 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Design of a transonically profiled wing

    Kiekebusch, B. | NTRS | 1978


    Method of and Transonically Operating Aircraft having Devices For Suppressing Aeroelastic Instabilities

    BACKHAUS KAI / ARNOLD JÜRGEN / HENNINGS HOLGER et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Profiled strip, system and method for producing a profiled strip

    ORTMUELLER MICHAEL / LANDECK DAVID | Europäisches Patentamt | 2019

    Freier Zugriff

    PROFILED REINFORCEMENT ELEMENT

    TESSIER BERNARD / PETRY DAVID | Europäisches Patentamt | 2018

    Freier Zugriff

    Profiled reinforcement element

    TESSIER BERNARD / PETRY DAVID | Europäisches Patentamt | 2021

    Freier Zugriff