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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 16

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 16 — 16 NACA RM A57K05 … $,deq (a) Cn vs. (3 Figure 4.- The variation of side force and of rolling-moment, yawing-moment, and pitching-moment coefficients with sideslip; M = 0.80, R = 0.5xl06.

NASA Technical Reports Server (NTRS)

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