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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 25

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 25 — 25 NACA RM A57K05 … Figure - The pitching-moment contribution of fuselage strakes with the wing on and with the wing off; M = 0.40, R = 0.9x10°. NACA - Langley Field, Va.

NASA Technical Reports Server (NTRS)

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