Biplane cellules using N.A.C.A.-M6 airfoil section tested in N.A.C.A. variable-density wind tunnel; three cellules differing in amount of stagger tested at two air densities; indications that positive stagger increases induced drag, decreases maximum lift at Reynolds numbers near full scale, and displaces moment coefficient in positive direction.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Preliminary biplane tests in the variable density wind tunnel


    Weitere Titelangaben:

    Nat. Advisory Committee Aeronautics -- Tech. Note


    Beteiligte:


    Erscheinungsdatum :

    1928


    Format / Umfang :

    15 pages


    Anmerkungen:

    7 Figs. on Supp. plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Wind tunnel tests on a fokker biplane

    Cowley, W. L. | TIBKAT | 1923


    Wind tunnel pressure distribution tests on series of biplane wing models

    Knight, M. / Noyes, R.W. | Engineering Index Backfile | 1929


    Wind tunnel pressure distribution tests on a series of biplane wing models

    Knight, Montgomery ;Noyes, Richard W. | SLUB | 1929