DescriptionPressure gradient profile plots above a wing.png
English: The plot shows the pressure gradient at eight locations above the wing for alpha=3, 4096x2048 gird 2-D airflow simulation case from Swanson, R. and Langer, S., “Comparison of NACA 0012 Laminar Flow Solutions: Structured and Unstructured Grid Methods,” NASA/TM-2016-219003.
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Captions
Plots of the pressure gradient profiles for eight locations above the wing.