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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 33

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 33 — Ou … Figure 10.— The aerodynamic characteristics of the two wings at various Mach numbers, based upon exposed—wing loads plus load over fuselage in vicinity of the wing.

NASA Technical Reports Server (NTRS)

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