The results of an aircraft wing design study are reported. The selected study airplane configuration is defined. The suction surface, ducting, and compressor systems are described. Techniques of manufacturing suction surfaces are identified and discussed. A wing box of graphite/epoxy composite is defined. Leading and trailing edge structures of composite construction are described. Control surfaces, engine installation, and landing gear are illustrated and discussed. The preliminary wing design is appraised from the standpoint of manufacturing, weight, operations, and durability. It is concluded that a practical laminar flow control (LFC) wing of composite material can be built, and that such a wing will be lighter than an equivalent metal wing. As a result, a program of suction surface evaluation and other studies of configuration, aerodynamics, structural design and manufacturing, and suction systems are recommended. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A Preliminary Design Study of a Laminar Flow Control Wing of Composite Materials for Long Range Transport Aircraft


    Beteiligte:
    G. R. Swinford (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    125 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Aircraft energy efficiency laminar flow control wing design study

    Bonner, T. F., Jr. / Pride, J. D., Jr. / Fernald, W. W. | NTRS | 1977


    Aircraft Energy Efficiency Laminar Flow Control Wing Design Study

    T. F. Bonner / J. D. Pride / W. W. Fernald | NTIS | 1977


    AIRCRAFT WING OR EMPENNAGE PANEL FROM LAMINAR COMPOSITE MATERIALS

    VASILEV VALERIJ VITALEVICH / PALKIN ALEKSANDR NIKOLAEVICH / SISAURI VITALIJ IRAKLIEVICH et al. | Europäisches Patentamt | 2020

    Freier Zugriff