Formulas and curves are given for elliptic, straight tapered and trapezoidal wings, based on modified form of Schrenk distribution of lift; comparison with experimental curves for derivatives shows that method gives good agreement and enables reasonably accurate estimation of rolling performance of aircraft to be made.


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    Title :

    Rolling performance of aircraft


    Additional title:

    Aircraft Eng


    Contributors:
    Roberts, H. (author)

    Published in:

    Aircraft Engineering ; 20 , n 232 ; p 167-170 + 181


    Publication date :

    1948


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Rolling Performance of Aircraft

    Roberts, H. | Emerald Group Publishing | 1948


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