Date: 2013-07-16 07:29:23Fluid mechanics Airfoil Supercritical airfoil Boundary layer Laminar flow Pressure coefficient Flow separation Lift Shock wave Aerospace engineering Aerodynamics Fluid dynamics | | 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 ListSource URL: crgis.ndc.nasa.govDownload Document from Source Website File Size: 99,71 KBShare Document on Facebook
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