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The document presents preliminary results from wind tunnel tests of a 5.2% scale model of the Common Research Model with Natural Laminar Flow (CRM-NLF) conducted at NASA Langley Research Center. The tests aimed to validate the Crossflow Attenuated Natural Laminar Flow (CATNLF) design method, which shapes airfoils to delay transition on swept wings, and to characterize the testing capabilities of the National Transonic Facility. Preliminary findings indicate that the CATNLF method successfully delays transit

Author

trongnghia13092018

Language

EN