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Flight Measurements with the Douglas D-558-II (buaero No. 37974) Research Airplane : Measurements of Wing Loads at Mach Numbers up to 0.87 (1950)
NASA Technical Reports Server (NTRS) · leaf 28
ro CD … Wing PaneI Norma! Force Coefficient, C/\jwp Figure 10.- Variation of wing-panel bending-moment coefficient with wing- panel normal-force coefficient.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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