Problems of high aspect ratio wings, with specific reference to Hurel-Dubois strutted wing, developed in France by M.HUREL; comparison of H.D.32 with cantilever aircraft of normal aspect ratio having same wing area and approximately same takeoff and landing weight, demonstrating emphatically superiority of Hurel's theories, in so far as pure economy of transport is considered. English translation from Luftfahrttechnik Aug 1955.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design for wing efficiency


    Weitere Titelangaben:

    Aeroplane


    Beteiligte:
    Stender, W. (Autor:in)

    Erschienen in:

    Aeroplane ; 90 , n 2327 ; p 226-228


    Erscheinungsdatum :

    1956


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    SUBSONIC WING SPAN EFFICIENCY

    FROST, R. C. / RUTHERFORD, R. | AIAA | 1963


    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


    WING AND WING DESIGN METHOD

    NOMURA TAKAYUKI / KODAMA SATOSHI / YUMITORI TAKAAKI et al. | Europäisches Patentamt | 2020

    Freier Zugriff