Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
Details
- OL Work ID
- OL11173817W
Subjects
Drag reductionSurface roughness effectsWind tunnel testsSwept wingsLaminar boundary layerBoundary layer controlBoundary layer transitionTurbulence effects