Tests of aerodynamically heated multiweb wing structures in a free jet at Mach number 2: two aluminum-alloy models of 20-inch chord with 0.064- and 0.081-inch-thick skin
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Tests of aerodynamically heated multiweb wing structures in a free jet at Mach number 2: two aluminum-alloy models of 20-inch chord with 0.064- and 0.081-inch-thick skin, report, August 9, 1955; (digital.library.unt.edu/ark:/67531/metadc61471/: accessed April 26, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.