Aeroelastic tailoring analysis for preliminary design of advanced turbo propellers with composite blades
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[1] P. Friedmann,et al. Structural dynamic modeling of advanced composite propellers by the finite element method , 1987 .
[2] Hermann J. Hassig,et al. An Approximate True Damping Solution of the Flutter Equation by Determinant Iteration , 1971 .
[3] E. C. Yates,et al. Modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speeds. , 1966 .