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F-16XL Ship #2 Supersonic Laminar Flow Control experiment

F-16XL Ship #2
NASA's two-seat F-16XL #2 research aircraft is shown in the modification hangar at the Dryden Flight Research Center, Edwards, CA, during installation of a titanium "glove" on the upper surface of its modified left wing.

EC95-43003-1
NASA’s two-seat F-16XL #2 research aircraft is shown in the modification hangar at the Dryden Flight Research Center, Edwards, CA, during installation of a titanium “glove” on the upper surface of its modified left wing.
The aircraft subsequently concluded a 13 month-long, 45-flight research program which investigated drawing off a small portion of the boundary-layer air to provide laminar – or smooth – flow over a major portion of a wing flying at supersonic speeds. A turbo-compressor in the aircraft’s fuselage provided suction to draw air through more than 10 million tiny laser-drilled holes in the glove via a manifold system employing 20 valves.
Data obtained during the program could assist designers of future high-speed aircraft in developing a more efficient civil transport.March 10, 1995NASA Photo › F-16XL-2 Project Description