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 20
a, deg .3 .2 .1 0 -.1 Cm Figure 5.- The effects of several tip-tank fin arrangements on the low-speed lift and pitching- moment characteristics; M = 0.40, R = 0.9xl06, it = -5°*
NASA Technical Reports Server (NTRS)
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