Two methods of obtaining balancing effect are explained, (1) by moving pivot points aft to center of pressure about 20 per cent aft leading edge on rectangular surface, and (2) by moving center of pressure forward to pivot or hinge line by extension of part of surface in front of hinge line.


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    Title :

    Balanced control surfaces on aircraft


    Additional title:

    Aviation


    Contributors:
    Wing, R.N. (author)

    Published in:

    Aviation ; 8 , n 2 ; p 57-58


    Publication date :

    1920


    Size :

    2 pages


    Remarks:

    4 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Balanced and servo control surfaces

    Engineering Index Backfile | 1930


    Balanced and servo control surfaces

    Engineering Index Backfile | 1930




    Balanced on Air Aircraft

    J. Reeves | NTIS | 1994