...Flutter Suppression of a Wing Section in a Compressible Flow
𝐽0J0 and 𝐽1J1 are Bessel functions of the first kind of order 0 and 1, respectively, 𝑧=𝑀∞𝑠|𝑥−𝜉|𝑖𝛽2z=M∞sx−ξiβ2, 𝑀∞M∞ the freestream Mach number, 𝛽2=1−𝑀2∞β2=1−M∞2 and the functions 𝐺0G0 and 𝐺1G1, are 𝐺0(𝑧)...