An oscillating wing with control surfaces in two-dimensional, compressible, subsonic flow is investigated. Computed numerical results are given for the forces and moments, useful for flutter calculations.


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    Title :

    Zur Stabilitaet des schwingenden Tragfluegels im Unterschallbereich (Stability of an Oscillating Wing in Subsonic Range)


    Contributors:
    F. Wille (author)

    Publication date :

    1969


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English