1. n 294 p 14-16: Paper reports on work done at RAE, Farnborough, and British aircraft firms on some specifically aerodynamic problems; attempt is made to explain dominant and typical aerodynamic problems and how these can be solved; paper is restricted to slender wings of predominantly light-alloy construction with turbojet engines, to cruise at about twice speed of sound. 2. n 295 p 14-19: Design of volume distribution, and limitations and boundaries to flight regime; diagrams.


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    Title :

    Slender wings for supersonic flight


    Additional title:

    Shell Aviation News


    Contributors:

    Published in:

    Publication date :

    1962


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English