This report deals with the results of tests on struts conducted at Washington Navy Yard. Two models of the modified Navy strut, no. 1, were tested in the 8 by 8 foot wind tunnel. The tests were made to determine the total resistance end effect and the pressure distribution at various wind-tunnel speeds with the length of the strut transverse to the current. Only the measurements made at zero pitch and yaw are given in this report.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Point drag and total drag of navy struts no. 1 modified


    Beteiligte:
    Zahm, A F (Autor:in) / Smith, R H (Autor:in) / Hill, G C (Autor:in)

    Erscheinungsdatum :

    1923-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Interference effects and drag of struts on a monoplane wing

    Ward, K.E. | Engineering Index Backfile | 1931




    Hydrodynamic drag of 12- and 21-percent-thick surface-piercing struts

    Coffee, Jr., C.W. / McKann, R.E. | Engineering Index Backfile | 1953


    Hydrodynamic Drag of 12- and 21-percent-thick Surface-piercing Struts

    Coffee, Claude W , Jr / Mckann, Robert E | NTRS | 1953