Revision history of "Nov 27 1972"

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• (cur) (last) 04:04, 15 December 2009 RobertG (Talk | contribs) (5,247 bytes) (New page: NASA's TF-8A aircraft, equipped with supercritical wing and new fuselage fairings, was flight-tested at constant dynamic pressure of 9580 newtons per sq m (200 psf). Pressure distribution ...)

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