Horizontal-tail Load Measurements at Transonic Speeds of the Bell X-1 Research Airplane (1953)
NASA Technical Reports Server (NTRS) · leaf 19
18 NACA RM L53F30 CONFIDENTIAL -p 2 O Transonic M 0.91 -o -.05 … Figure 5*- Typical variation of tail normal-force coefficient with airplane normal-force coefficient during pull-ups; center of gravity at 23-55 per- cent mean aerodynamic chord. Bell X-l airplane. CONFIDENTIAL
NASA Technical Reports Server (NTRS)
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