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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    Title :

    Design study for supersonic airliner


    Additional title:

    Engineering


    Contributors:
    Newell, A.F. (author) / Howe, D. (author)

    Published in:

    Engineering ; 193 , n 5008


    Publication date :

    1962


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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