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Published in 2021 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2021.107043
Abstract: Abstract A Reynolds-averaged Navier-Stokes solver has been equipped with two different transition prediction and modeling techniques for automatic transition prediction on general three-dimensional geometrical configurations. The first technique is a streamline-based approach that applies an…
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Keywords:
simplified fuselage;
model;
three dimensional;
configuration ... See more keywords