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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    Title :

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


    Contributors:

    Publication date :

    1957-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






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