Wind-tunnel investigation of the low-speed longitudinal and lateral control characteristics of a triangular-wing model of aspect ratio 2.31 having constant-chord control surfaces
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Wind-tunnel investigation of the low-speed longitudinal and lateral control characteristics of a triangular-wing model of aspect ratio 2.31 having constant-chord control surfaces, report, September 6, 1950; (digital.library.unt.edu/ark:/67531/metadc58555/: accessed April 24, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.