Aerodynamic aspects of engine air intake for Anglo-French Concorde aircraft; mounted under wing of Concorde, inlet is divided to provide independent supplies of air to pair of engines, specific arrangement that introduces particular problems in allowing for wing flow-field and avoiding interaction between twin inlets; factors considered in choice of compression system and intake geometry; aerodynamic and other development tests required to make appropriate decisions are described showing suitability of basic geometry in association with other components of propulsion system for SST operation. (13357)


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    Titel :

    Design and development of air intake for supersonic transport aircraft


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Rettie, I.H. (Autor:in) / Lewis, W.G.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch






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