Semi-empirical indicial response model for a 65 deg delta wing oscillating in roll

Select Means for Determining Unsteady Aerodynamic Response Characteristics from Static Data

“…Along this same vein, the analysis of Grismer and Jenkins and the models of Myatt and Graham 14 assumed that the unsteady rolling moment of the 65° delta wing undergoing harmonic and ramp-and-hold motions could be divided into two components. The first component was given by the potential flow about the wing.…”