Theoretical results for the initial lift-curve slope of straight-tapered wings, based on the linearized equations of inviscid motion, have been evaluated and are presented in the form of graphs.


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    Title :

    Lift-Curve Slope at Subsonic and Supersonic Speeds


    Subtitle :

    Graphical Presentation of Theoretical Results for Straight-Tapered Wings


    Contributors:

    Published in:

    Publication date :

    1954-08-01


    Size :

    14 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English