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 52
VJ1 ro … Figure 10.- Change in lateral stability derivatives due to torsional flexibility of the vertical stabilizer in configurations C and D. Estimates based on calculated derivatives.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
