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- W2140400269 abstract "A near-surface-mounted hot-wire shear gauge was designed, built, and installed in three locations on the upper surface of an NACA 0012 airfoil. The time constant of the gauge is essentially the same as a hot-wire anemometer, which implies that the gauge can measure turbulent shear stress. The skin friction at these three locations was measured over a reduced frequency range of 0-6.4 at two angles of attack (0 and 10 deg)" @default.
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- W2140400269 date "1992-11-01" @default.
- W2140400269 modified "2023-10-16" @default.
- W2140400269 title "Unsteady turbulent skin-friction measurement in an adverse pressure gradient" @default.
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- W2140400269 doi "https://doi.org/10.2514/3.11280" @default.
- W2140400269 hasPublicationYear "1992" @default.
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