Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment /

Runyan, Harry L.
United States. National Advisory Committee for Aeronautics.

Publication date

January 1951

Publisher

Washington, D.C. : National Advisory Committee for Aeronautics,

Abstract

The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented in this report. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter.NACA TN No. 2396."July 1951."Includes bibliographical references.The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented in this report. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter.Mode of access: Internet

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Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment /

Abstract

Extracted data

Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment /

Abstract

Extracted data

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