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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 32
uo ro … C/Vwp (b) Slats unlocked. (a) Slats locked. Figure lh.- Variation of wing-panel pitching-moment coefficient Cu VcWP/4 NACA RM L50H16 with wing-panel normal-force coefficient at high normal-force coeffi- cients.NASA Technical Reports Server (NTRS)
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