Aerodynamic Characteristics of NACA RM-10 Missile in 8- by 6-foot Supersonic Wind Tunnel at Mach Numbers from 1.49 to 1.98 II : Presentation and Analysis of Force Measurements (1950)
NASA Technical Reports Server (NTRS) · leaf 29
28 NACA RM E50D28 … (b) Pitching-moment coefficient. Figure 7. - Continued. Variation of aerodynamic characteristics with angle of attack at four Mach numbers for body plus four fins.
NASA Technical Reports Server (NTRS)
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