Numerical Simulations of the F-16XL at Flight-Test Conditions using Delayed Detached-Eddy Simulation.

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This study documents the use of the Kestrel flow solver with its solution-based mesh refinement capability and delayed detached-eddy simulation turbulence models for F-16XL flight condition 25, which is a subsonic high-angle-of-attack flight condition that has proven particularly challenging for computational researchers.

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