NASA NTRS · 19720016344
Wind tunnel test data for wing trailing vortex flow survey
Abstract
Data are presented on velocity measurements made with hot wire anemometers in the wake of a model of the CV-990 aircraft and a rectangular wing in the NASA-Ames 2.14x3.05 meter (7- by 10-foot) wind tunnels. Variables included angle of attack, tunnel speed and axial distance up to 12 chord lengths downstream from the wing trailing edge. Effects of deflecting trailing edge flaps and small spoiler panels are shown.
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Chigier, N. A., Corsiglia, V. R.. 1972-05-01. Wind tunnel test data for wing trailing vortex flow survey. https://ntrs.nasa.gov/citations/19720016344
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