Whilst all published information on the arrow wing concept for future Supersonic Transport designs has, in general, placed considerable importance on the benefits of this particular layout, we should now be investigating ways and means in which the theorising and experimenting may be supplanted by active in-flight research.


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    Title :

    The Arrow Wing


    Subtitle :

    Its potentialities and drawbacks with regard to in-flight aerodynamic research


    Contributors:


    Publication date :

    1977-08-01


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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