College of Aeronautics at Cranfield has made design study of Mach 2.2 civil air transport different from any proposed by industry; it is known as A-60, and is for transatlantic route; tailless, slender integrated layout chosen, makes it difficult to incorporate cabin windows; planform is basically 73 delta with curved leading edge in region of tips and roots; 6 turbojet engines, of 18,000 lb sea level static thrust, are mounted in rear fuselage; diagrams. From paper before Instn Production Engrs.


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    Titel :

    Design study for supersonic airliner


    Weitere Titelangaben:

    Engineering


    Beteiligte:
    Newell, A.F. (Autor:in) / Howe, D. (Autor:in)

    Erschienen in:

    Engineering ; 193 , n 5008


    Erscheinungsdatum :

    1962


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Supersonic Airliner Problems

    Emerald Group Publishing | 1959


    Britain's supersonic airliner

    Cownie, J.R. | Engineering Index Backfile | 1959


    Case against supersonic airliner

    Lundberg, B. | Engineering Index Backfile | 1962


    Conceptual Design of an N+2 Supersonic Airliner

    Hamel, L. / Folk, T. / Jimenez, H. et al. | British Library Conference Proceedings | 2009


    Two significant technique requirements in supersonic airliner design

    Chongwen, J. / Jun, H. / Yihua, C. | British Library Online Contents | 2005