Horizontal-tail Load Measurements at Transonic Speeds of the Bell X-1 Research Airplane (1953)
NASA Technical Reports Server (NTRS) · leaf 16
NACA RM L53F30 CONFIDENTIAL 15 … 0 1 2 3 h Time, t, sec (a) Subsonic, M » 0-70; hp « 14,000 feet. Figure 4.- Typical time history of a pull-up for evaluation of tail loads. Bell X-l airplane. CONFIDENTIAL
NASA Technical Reports Server (NTRS)
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