Tests made in 7- by 10-ft wind tunnel with 4-by 8-ft wing hinged at tunnel jet boundary and restrained in roll by elastic cords; time histories were taken of motion of control device under test and resulting wing motion.


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    Title :

    Development of N.A.C.A. Slot-lip aileron


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Weick, F.E. (author) / Shortal, J.A. (author)


    Publication date :

    1935


    Size :

    10 pages


    Remarks:

    19 Supp plates


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Development of the NACA slot lip [aileron]

    Weick, Fred E. ;Shortal, Joseph A. | SLUB | 1935


    Experiments on airfoils with aileron and slot

    Betz, A. | Engineering Index Backfile | 1927


    Full-scale tests of new type N.A.C.A. nose-slot cowling

    Theodorsen, T. / Brevoort, M.J. / Stickle, G.W. et al. | Engineering Index Backfile | 1937


    Full-scale tests of new type N.A.C.A. nose-slot cowling

    Theodorsen, T. / Brevoort, M.J. / Stickle, G.W. et al. | Engineering Index Backfile | 1937


    Full-scale tests of new type N.A.C.A. nose-slot cowling

    Theodorsen, T. / Brevoort, M.J. / Stickle, G.W. et al. | Engineering Index Backfile | 1937