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- W2123146811 abstract "Results from an experimental investigation of asymmetric trailing-edge flows at high Reynolds numbers and subsonic Mach numbers are presented. Measurements include skin friction; surface and flow-field pressures; and mean-velocity, turbulent shear-stress, and turbulent kinetic-energy profiles in the trailing-edge region. Comparisons are made with computed solutions using Reynolds averaged Navier-Stokes and boundary-layer equations; two different turbulence models are used. Two attached flow are considered, one having a moderate adverse pressure gradient and the other a more severe gradient. From the comparisons, an evaluation is made of the predictions for these two pressure-gradient cases. Although the comparisons demonstrate reasonable agreement for the moderate pressure-gradient case, some differences are noted for the severe pressure-gradient case." @default.
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- W2123146811 date "1980-07-14" @default.
- W2123146811 modified "2023-10-05" @default.
- W2123146811 title "Asymmetric trailing-edge flows at high Reynolds number" @default.
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- W2123146811 doi "https://doi.org/10.2514/6.1980-1396" @default.
- W2123146811 hasPublicationYear "1980" @default.
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