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Investigation of Horn Balances on a 45 Degree Sweptback Horizontal Tail Surface at High Subsonic Speeds (1948)

NASA Technical Reports Server (NTRS) · leaf 21

An illustration from Investigation of Horn Balances on a 45 Degree Sweptback Horizontal Tail Surface at High Subsonic Speeds, 1948, leaf 21
NACA EM No. l8J01 20 … /i/7^/^ of (Ty Figure 5-- Aerodynamic characteristics of the 45° swepthack horizontal- tail model equipped with the large horn. M = 0.30. CONFIDENTIAL

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