Airfoil Technology The historical evolution of airfoil sections, [removed]The last two shapes are low-drag sections designed to have laminar flow over 60 to 70 percent of chord on both the upper and lower surface. Th - Supercritical airfoil - Document - PDFSEARCH.IO

First Page	Meta Content
	Airfoil Technology The historical evolution of airfoil sections, [removed]The last two shapes are low-drag sections designed to have laminar flow over 60 to 70 percent of chord on both the upper and lower surface. Th Add to Reading List Document Date: 2014-08-11 17:14:13 Open Document File Size: 119,25 KB Share Result on Facebook Company National Physical Laboratory / / Country United States / / Currency pence / / Facility Eiffel Tower / Langley Research Center / Royal Aircraft Factory / National Physical Laboratory / Variable-Density Wind Tunnel / / IndustryTerm moderate travel / / OperatingSystem XP / / Organization National Aeronautics and Space Administration / British government / Royal Air Force / Advisory Committee on Aeronautics / Langley Research Center / / Person Richard T. Whitcomb / Alexandre Gustave Eiffel / / Product B-17 Flying Fortress / Mustang / DC-3 / P-51 Mustang / Beechcraft Bonanza / / ProvinceOrState Virginia / / Technology Airfoil Technology / / URL http / SocialTag NACA airfoil Airfoil Supercritical airfoil Camber Foil Lift National Advisory Committee for Aeronautics Center of pressure Angle of attack Aerodynamics

Airfoil Technology The historical evolution of airfoil sections, [removed]The last two shapes are low-drag sections designed to have laminar flow over 60 to 70 percent of chord on both the upper and lower surface. ThAdd to Reading List