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- W1982522884 abstract "A laser velocimeter (LV) surveyed the flow above two stalled wings. Each wing was tested in a different wind tunnel at different Mach numbers. The low-Mach-number test had an angle of attack of 19.4 deg, 0.15 Mach number, and 1 x 1,000,000 Reynolds number. The mean velocities above the reversed, separated flow were closely modeled by error function profiles. Thus, the flow resembled a turbulent free-shear layer. The high-Mach-number test had an angle of attack of 19.5 deg, 0.49 Mach number, and 1,400,000 Reynolds number. A series of strong, discrete vortices were shed from the airfoil crest at regular intervals. Both tests demonstrated the importance of the unsteady part of the velocities." @default.
- W1982522884 created "2016-06-24" @default.
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- W1982522884 date "1979-01-15" @default.
- W1982522884 modified "2023-09-23" @default.
- W1982522884 title "Comparison of two flow surveys above stalled wings" @default.
- W1982522884 doi "https://doi.org/10.2514/6.1979-147" @default.
- W1982522884 hasPublicationYear "1979" @default.
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