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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 33

An illustration from 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, leaf 33 — cn … Cna (a) Slats locked. (b) Slats unlocked. Figure 15.- Variation of wing-panel pitching-moment coefficient C™ ^c/k with airplane normal-force coefficient at high normal-force coeffi- cients . uo uo

NASA Technical Reports Server (NTRS)

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