The final design of a hypersonic, SCRAMjet research aircraft, which is to be dropped from a carrier plane, is considered. Topics such as propulsion systems, aerodynamics, component weight analysis, and aircraft design with waverider analyses are stressed with smaller emphasis placed on aircraft systems such as cockpit design and landing gear configurations. Propulsion systems include analysis of the turbofanramjet for acceleration to low hypersonic speed (Mach 6.0) and analysis of the SCRAMjets themselves to carry the aircraft to Mach 10.0. Both analyses include the use of liquid hydrogen as fuel. Inlet design for both propulsion systems is analyzed as well. Aerodynamic properties are found using empirical and theoretical formulas for lift and drag on delta-wing aircraft. The aircraft design involves the integration of all preliminary studies into a modified waverider configuration.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Stb-White


    Beteiligte:
    D. Molnar (Autor:in) / R. Ammon (Autor:in) / T. Gallagher (Autor:in) / P. Gouhin (Autor:in) / S. Hermann (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    167 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    White box

    LIU BAOPING / ZHAO WEI / HU XIAOMEI et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    White Noise

    Huber, Angelika | Online Contents | 2011


    White Topping

    Powell, J. | British Library Conference Proceedings | 2003


    White horse

    Engineering Index Backfile | 1942


    White dwarfs

    Barstow, M.A. | Elsevier | 1991