Investigation of the effect of spanwise positioning of a vertically symmetric ogive-cylinder nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6 with and without a fuselage
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Investigation of the effect of spanwise positioning of a vertically symmetric ogive-cylinder nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6 with and without a fuselage, report, October 7, 1953; (digital.library.unt.edu/ark:/67531/metadc59744/: accessed April 24, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.