Design and development of supersonic research aircraft, with delta wing plan form of aspect ratio 2, having Rolls-Royce "RA5" engine in body; design matters of interest are: drooping nose, main undercarriage, engine installation, hydraulics and power controls; manufacturing problems. From lecture before Roy Aeronautical Soc. (See also Engineer v 203 n 5274 Feb 22 1957 p 297-9; Flight v 71 n 2509, 2510 Feb 22 1957 p 235-7, Mar 1 p 266-7)


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    Title :

    Fairey "Delta 2"


    Additional title:

    Shell Aviation News


    Contributors:
    Lickley, R.L. (author) / Twiss, L.P. (author)

    Published in:

    Publication date :

    1957


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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