Time-vector Determined Lateral Derivatives of a Swept-wing Fighter-type Airplane with Three Different Vertical Tails at Mach Numbers Between 0.70 and 1.48 (1956)
NASA Technical Reports Server (NTRS) · leaf 74
(a) Amplitude ratio characteristics. Figure 25.- Amplitude ratio and phase angle characteristics of the air- plane at its natural frequency as functions of Mach number, altitude, and angle of attack per load factor. Configuration C. CONFIDENTIAL
NASA Technical Reports Server (NTRS)
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