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Subsonic Aerodynamic Characteristics up to Extreme Angles of Attack of an Airplane Model Having an Unswept Wing and a High Horizontal Tail (1958)

NASA Technical Reports Server (NTRS) · leaf 21

An illustration from Subsonic Aerodynamic Characteristics up to Extreme Angles of Attack of an Airplane Model Having an Unswept Wing and a High Horizontal Tail, 1958, leaf 21 — NACA RM A57K05 21 … a, deg Figure 6.- Effects of adding tip tanks and tip-tank fins on the pitching- moment characteristics and on the pitching moment contributed by the horizontal tail; M = 0.4, R = 0.9xl06.

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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