51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013
DOI: 10.2514/6.2013-985
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RANS Simulations of Flows with Shock Wave-Boundary Layer Interaction

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Cited by 5 publications
(2 citation statements)
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“…Still, the complexity of the optimized geometry and the associated flow field raise some questions on the validity of the optimized solution. In particular, as demonstrated in Vieira and Azevedo [142], who compared four different turbulent closures, in presence of a strong shock boundary layer interaction RANS may not predict the flow correctly at the foot of the shock. Michelassi [82] showed that, while the shock strength and position may be captured correctly, the separation at the foot of a strong shock in presence of a downstream adverse pressure gradient was not captured accurately.…”
Section: High-pressure Compressormentioning
confidence: 97%
“…Still, the complexity of the optimized geometry and the associated flow field raise some questions on the validity of the optimized solution. In particular, as demonstrated in Vieira and Azevedo [142], who compared four different turbulent closures, in presence of a strong shock boundary layer interaction RANS may not predict the flow correctly at the foot of the shock. Michelassi [82] showed that, while the shock strength and position may be captured correctly, the separation at the foot of a strong shock in presence of a downstream adverse pressure gradient was not captured accurately.…”
Section: High-pressure Compressormentioning
confidence: 97%
“…Meshes composed mainly of hexahedral elements were developed in previous work 6 for the various test cases. A half domain mesh is used, which is justifiable by the hypothesis that a symmetric flow takes place.…”
Section: Iia Test Cases and Computational Gridsmentioning
confidence: 99%