This model was tested in the 0.3m Transonic Cryogenic Tunnel ( Bldg[removed]in the[removed]timeframe. Two technologies were merging that inspired the contour of the airfoil. First, the LaRC LFC program (Laminar Flow C - Flow separation - Document - PDFSEARCH.IO

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	This model was tested in the 0.3m Transonic Cryogenic Tunnel ( Bldg[removed]in the[removed]timeframe. Two technologies were merging that inspired the contour of the airfoil. First, the LaRC LFC program (Laminar Flow C Add to Reading List Document Date: 2013-07-16 07:29:23 Open Document File Size: 99,71 KB Share Result on Facebook Facility Transonic Cryogenic Tunnel / Foot Transonic Pressure Tunnel / Inch Transonic Airfoil Tunnel / / Organization Department of Defense / / Product swept wing / / Technology Two technologies / Flow Control / / SocialTag Fluid mechanics Airfoil Supercritical airfoil Boundary layer Laminar flow Pressure coefficient Flow separation Lift Shock wave Aerospace engineering

This model was tested in the 0.3m Transonic Cryogenic Tunnel ( Bldg[removed]in the[removed]timeframe. Two technologies were merging that inspired the contour of the airfoil. First, the LaRC LFC program (Laminar Flow CAdd to Reading List