Calculation of the Aeroelastic Characteristics of a Wing during Vibrations in a Subsonic Flow by the Discrete Singularity Method
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DOI: 10.1134/s0036029520100201
Abstract: The problem of determining the total and generalized aerodynamic forces for an airplane wing during vibrations in a compressible flow with allowance for the real frequencies of its natural vibrations is considered. The need to… read more here.
Keywords: wing vibrations; subsonic flow; aeroelastic characteristics; vibrations subsonic ... See more keywords