Models having aspect ratios ranging from 2 to 13 were tested at Mach numbers up to 0.92; examination of data is made on basis of reference theoretical values obtained from 2-dimensional incompressible flow theory; on this basis reduction in aspect ratio increased ratio of experimental to calculated flutter speed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Experimental investigation of effect of aspect ratio and Mach number on flutter of cantilever wings


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1960


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Initial Experiments on Flutter of Unswept Cantilever Wings at Mach Number 1.3

    Tuovila, W J / Baker, John E / Regier, Arthur, A | NTRS | 1954


    Initial experiments on flutter of unswept cantilever wings at mach number 1.3

    Tuovila, W. J. / Beker, John E. / Regier, Arthur A. | TIBKAT | 1954


    Initial Experiments on Flutter of Unswept Cantilever Wings at Mach Number 1.3

    Tuovila, W J / Baker, John E / Regier, Arthur A | NTRS | 1949


    Initial experiments on flutter of unswept cantilever wings at mach number 1.3

    Tuovila, W.J. / Baker, J.E. / Regier, A.A. | Engineering Index Backfile | 1954