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 24
NACA RM A57K05 24 … a, deg Figure 8.- The variation with angle of attack of the contribution of the tail to dCjn/da with the wing on and with the wing off; R = 0.5x10s, it = -5°.
NASA Technical Reports Server (NTRS)
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