As preliminary to investigating effect of flaps on swept back wings, it was necessary to devise satisfactory method by which Glauert solution could be accurately and readily evaluated for wing of arbitrary plan form with discontinuities of incidence; report demonstrates new method which, given standard solutions which are readily computed from simple formulas, involves scarcely more work than in application of Glauert solution to wing without discontinuities of incidence.


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    Title :

    Glauert loading of wings with discontinuities of incidence


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1946


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :