NASA NTRS · 19760003925
Wing Tip Vortex Drag
Abstract
Optimization of L/D through minimizing induced drag through a detailed flow study together with force, pressure and vorticity measurements is considered. Flow visualization with neutral helium bubbles provides an excellent means of observing the effects of configuration changes.
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Muirhead, V. U.. 1975-01-01. Wing Tip Vortex Drag. https://ntrs.nasa.gov/citations/19760003925
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