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Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel

Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel

W. S. Saric

Details

OL Work ID
OL11173817W

Subjects

Drag reductionSurface roughness effectsWind tunnel testsSwept wingsLaminar boundary layerBoundary layer controlBoundary layer transitionTurbulence effects

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