Equations of motion for airplane with number of spherical fuel tanks are derived and are applied to two cases with two fuel tanks located in plane of symmetry; calculated motions show that airplane motion may be greatly changed by considering motion of fuel and, in particular, that small amplitude residual oscillations may result.


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    Title :

    Theoretical analysis of effect of fuel motion on airplane dynamics


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Schy, A.A. (author)


    Publication date :

    1951


    Size :

    53 pages


    Remarks:

    Charts, Tables


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Theoretical analysis of effects of fuel motion on airplane dynamics

    Schy, A.A. | Engineering Index Backfile | 1952




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