An experimental setup has been developed to study the wing-nacelle interaction of commercial transports during transonic operation. This stand allows the measurement of the overall loads, pressure distribution on the model, and velocities in the field by laser velocimetry. The analysis gives a better understanding of the wing-nacelle interaction and provides the best comparative elements for modeling calculations.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Analyse Detaillee de l'Interaction Voilure-Nacelle d'UN Avion de Transport Civil (Detailed Analysis of Wing-Nacelle Interaction for Commercial Transport Aircraft)


    Beteiligte:
    J. L. Godard (Autor:in) / O. Jacquotte (Autor:in) / D. Gisquet (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Nacelle-wing integration aspects for the high-speed civil transport aircraft

    Mavris, D. N. / Roehl, P. / Confederation of European Aerospace Societies | British Library Conference Proceedings | 1995



    ENGINE NACELLE ON AIRCRAFT WING

    BOLSUNOVSKIJ ANATOLIJ LONGENOVICH / BUZOVERYA NIKOLAJ PETROVICH / BRAGIN NIKOLAJ NIKOLAEVICH et al. | Europäisches Patentamt | 2017

    Freier Zugriff


    AVION À NACELLE DÉPORTÉE AFFLEURANT LE SILLAGE DE L’AILE

    GONIDEC PATRICK / AGUIRRE MIGUEL ANGEL / TANTOT NICOLAS et al. | Europäisches Patentamt | 2022

    Freier Zugriff