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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 60

An illustration from Investigation of Horn Balances on a 45 Degree Sweptback Horizontal Tail Surface at High Subsonic Speeds, 1948, leaf 60
NACA EM No. LSJOI 6l … /7c//?7/^er^/V Figure 22.- Variation of lift and drag coefficients with Mach nvmiber. Faired horn, 6g =0°. CONFIDENTIAL

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