Longitudinal Characteristics at Transonic and Supersonic Speeds of a Rocket-propelled Airplane Model Having a 60 Degree Delta Wing and Low Swept Horizontal Tail (1955)
NASA Technical Reports Server (NTRS) · leaf 23
Figure 4.- Typical portion of time histories of Mach number, tail deflec- tion, lateral-force coefficient, and lift coefficient.
NASA Technical Reports Server (NTRS)
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