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 27
2 6 NACA RM L55F27 … (a) 6 = -4.7°. i ro (b) 6 = -1.1°. Figure 8.- Variation of exposed wing lift coefficient with angle of attack and Mach number.
NASA Technical Reports Server (NTRS)
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