Roll Damping for Projectiles Including Wraparound, Offset, and Arbitrary Number of Fins
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[1] John D. Nicolaides,et al. A Method of Determining Some Aerodynamic Coefficients from Supersonic Free-Flight Tests of a Rolling Missile , 1950 .
[2] R. J. Yang,et al. An Improved Theoretical Aerodynamic Derivatives Computer Program for Sounding Rockets , 1979 .
[3] W. Oberkampf. Theoretical prediction of roll moments on finned bodies in supersonic flow , 1974 .
[4] D. Eastman. Roll Damping of Cruciform-Tailed Missiles , 1986 .
[5] C. W. Dahlke,et al. HYDRA 70 MK66 Aerodynamics and Roll Analysis , 1990 .
[6] Walter B. Sturek,et al. Computation of the roll characteristics of a finned projectile , 1996 .
[7] Sheo Prakash,et al. A simple estimation procedure of roll-rate derivatives for finned vehicles , 1984 .
[8] T. V. Lawson,et al. Wind tunnel investigations , 1978 .
[9] Gaynor J Adams,et al. Theoretical Damping in Roll and Rolling Moment Due to Differential Wing Incidence for Slender Cruciform Wings and Wing-Body Combinations , 1952 .