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AIAA AVIATION 2021 FORUM.
A wing-tail tandem configuration undergoing forced harmonic pitch is numerically simulated using Detached-Eddy Simulation (DES) coupled with an overset grid. This subjects a tail to a wing wake induced through forced pitch oscillations (Re=21,400, k=
Autor:
Tan, Kin Jon Benjamin
Wake phenomena and its encounter with downstream bodies are of engineering importance as it can affect aerodynamic loads. This can induce unfavourable-or even dangerous-conditions to aircraft through a loss of lift, or stability and control. Such sce
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https://explore.openaire.eu/search/publication?articleId=doi_________::aff6850867632c1a893159f8bc2904e1