The computing AGARD445.6 wing flutter results validate the physical law of a typical transonicflutter "dip" with the bottom near the domain which Mach number is 1.
Computation of wing flutter for unsteady transonic flows in the frequency domain is studied in this thesis.
本文研究了机翼跨音速颤振的频域计算方法。
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The unsteady aerodynamic results of the transonic wing are presented, and flutter calculation is made. The comparison with TDLM shows that the agreement is very good.