Physical argument behind methods developed at Royal Aircraft Establishment for reducing normal pressure drag of wings of moderate or large aspect ratio in transonic flight range; potential benefits of sweep; causes for drag forces arising; means of reducing drag.


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    Title :

    Methods of reducing transonic drag of swept-back wings at zero lift


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1957


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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