Since its original conception, project has grown from aircraft of 8600 lb all-up-weight with two 340-hp piston engines, to present turbine-powered Skyvan of 12,500-lb all-up-weight with two 666 ehp turbine engines; description of design philosophy as it applies to wing, flap, engine nacelles, rear fuselage, tail unit, flying controls and performance.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Short Turbo-Skyvan -- Aerodynamic design


    Weitere Titelangaben:

    Aircraft Eng


    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    SNECMA COUNTER ROTATING TURBO FAN AERODYNAMIC DESIGN LOGIC & TESTS RESULTS

    Talbotec, J. / Vernet, M. / International Council of the Aeronautical Sciences; Optimage Ltd | British Library Conference Proceedings | 2010



    Turbo Code Design for Short Blocks

    Jerkovits, Thomas / Matuz, Balazs | Deutsches Zentrum für Luft- und Raumfahrt (DLR) | 2016

    Freier Zugriff

    Short turbo-skyvan

    Emerald Group Publishing | 1965


    “Improving Aerodynamic Efficiency of Turbo is Our Key Focus”

    Springer India New Delhi | Springer Verlag | 2014