Tests showed that, although slot-tip ailerons did not have lag normally associated with plain spoilers, they were rather slow in developing full amount of rolling moment and therefore imparted sluggish motion to roll of airplane; tests in full scale tunnel showed that drag due to open slot was excessive, but tests in 7 by 10-ft tunnel revealed that drag could be reduced by modifying slot shape.


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    Titel :

    Wind-tunnel and flight tests of slot-tip ailerons


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Shortal, J.A. (Autor:in)


    Erscheinungsdatum :

    1937


    Format / Umfang :

    25 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




    Wind-tunnel and flight tests of slot-tip ailerons

    Shortal, J.A. | Engineering Index Backfile | 1937


    Wind-tunnel and flight tests of slot-tip ailerons

    Shortal, J.A. | Engineering Index Backfile | 1937


    Wind-tunnel and flight tests of slot-lip ailerons

    Shortal, Joseph A. | TIBKAT | 1937



    Wind tunnel tests on Junker type ailerons

    Bradfield, F. B. ;Wood, W. E. | SLUB | 1934