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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
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Document Date: 2013-07-16 07:29:23
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File Size: 99,71 KB
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Facility
Transonic Cryogenic Tunnel /
Foot Transonic Pressure Tunnel /
Inch Transonic Airfoil Tunnel /
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Organization
Department of Defense /
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Product
swept wing /
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Technology
Two technologies /
Flow Control /
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SocialTag
Fluid mechanics
Airfoil
Supercritical airfoil
Boundary layer
Laminar flow
Pressure coefficient
Flow separation
Lift
Shock wave
Aerospace engineering