Publication Date:
2017-10-02
Description:
Topics discussed include shear flow models, simplified models for treating separation, classical linear theory, a local linearization theory, a transonic linear theory, a transonic nonlinear theory, the experiment of Davis, and the experiment of Tijdeman. It is concluded that shear flow models, which have proven very accurate in taking into account boundary layer effects for panel flutter, are likely to be less so for lifting surface flutter. For many applications in transonic flow, transonic linear theory will be adequate.
Keywords:
AERODYNAMICS
Type:
AGARD Boundary Layer Effects on Unsteady Airloads; 28 p
Format:
text
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