The effectiveness and practicality of candidate leading edge systems for suction laminar flow control transport airplanes were investigated in a flight test program utilizing a modified JetStar airplane. The leading edge region imposes the most severe conditions on systems required for any type of laminar flow control. Tests of the leading edge systems, therefore, provided definitive results as to the feasibility of active laminar flow control on airplanes. The test airplane was operated under commercial transport operating procedures from various commercial airports and at various seasons of the year.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Simulated-Airline-Service Flight Tests of Laminar-Flow Control with Perforated-Surface Suction System


    Beteiligte:
    D. V. Maddalon (Autor:in) / A. L. Braslow (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    40 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Perforated surface for suction-type laminar flow control

    TIWARI SEAN / WEAVER LUBY | Europäisches Patentamt | 2018

    Freier Zugriff

    PERFORATED SURFACE FOR SUCTION-TYPE LAMINAR FLOW CONTROL

    TIWARI SEAN / WEAVER LUBY | Europäisches Patentamt | 2016

    Freier Zugriff

    PERFORATED SURFACE FOR SUCTION-TYPE LAMINAR FLOW CONTROL

    TIWARI SEAN / WEAVER LUBY | Europäisches Patentamt | 2017

    Freier Zugriff

    Laminar flow control leading-edge systems in simulated airline service

    Wagner, R. D. / Maddalon, D. V. / Fisher, D. F. | NTRS | 1990