1. Roll damping of cruciform-tailed missiles
2. A Method of Determining Some Aerodynamic Coefficients from Supersonic Free-Flight Tests of a Rolling Missile
3. 3Adams, G. J., and Dugan, D. W. "Theoretical Damping in Roll and Rolling Moment Due to Differential Wing Incidence for Slender Cruciform Wings and Wing-Body Combination," NACA Rept. 1088,1958.
4. 4Barrowman, J. S., Fan, D. N., Obosu, C. B., Vira, N. R., and Yang, R. J. "An Improved Theoretical Aerodynamic Derivatives Computer Program for Sounding Rockets," AIAA Paper 79-0504,1979.
5. Theoretical prediction of roll moments on finned bodies in supersonic flow