Abstract:We present high-fidelity numerical simulations of the interaction of an oblique shock impinging on the turbulent boundary layer developed over a rectangular flexible panel, replicating wind tunnel experiments by Daub et al. (AIAA Journal, vol. 54, 2016, pp. 670–678). The incoming free-stream Mach and unit Reynolds numbers are
$M_{\infty } = 3$
and
$Re_{\infty }=49.4\times 10^6 {\rm m}^{-1}$
, respectively. The reference boundary layer thickness upstream of… Show more
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