Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. Two airfoils fluttered at a Mach number of 0.85, a third airfoil fluttered at a Mach number of 1.03, and a fourth fluttered at a Mach number of 1.07. Results of calculations of flutter speed using incompressible and compressible air-force coefficients, including a Mach number of 1.0, are presented.


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    Titel :

    Results of Two Free-fall Experiments on Flutter of Thin Unswept Wings in the Transonic Speed Range


    Beteiligte:

    Erscheinungsdatum :

    01.01.1957


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch






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


    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