Test conducted at NASA Langley Research Center's Full Scale Tunnel in 1960. The researchers noted all the aerodynamic and structural deflection characteristics while also recording the buckling of the wings during the test. This is a short version of Langley Film #L-642. The full-length version is also available.
For more on the Full Scale Tunnel, see http://crgis.ndc.nasa.gov/historic/643.
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