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

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Date: 2013-07-16 07:29:23 Fluid 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 C Add to Reading List Source URL: crgis.ndc.nasa.gov Download Document from Source Website File Size: 99,71 KB Share Document on Facebook

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