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Comparison of the Aerodynamic Characteristics at Transonic Speeds of a Plane Wing and a Cambered and Twisted Wing, Both Having 45 Degrees of Sweepback and an Aspect Ratio of 6 (1953)

NASA Technical Reports Server (NTRS) · leaf 36

An illustration from Comparison of the Aerodynamic Characteristics at Transonic Speeds of a Plane Wing and a Cambered and Twisted Wing, Both Having 45 Degrees of Sweepback and an Aspect Ratio of 6, 1953, leaf 36 — Figure " - The liff coefficients of the complete model at various Mach numbers, for different horizontal stabilizer settings, 8. UU VJ1

NASA Technical Reports Server (NTRS)

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