Unsteady aerodynamic and aeroelastic computational test cases have been selected from the data set for the Benchmark Active Controls Technology model. Data sets for trailing-edge control surface oscillations and uppersurfacespoileroscillationsforarangeofMachnumbers, angleofattack, andstaticcontroldee ectionsareincluded. Cases also include static angles of attack, static trailing-edge control, and static upper-surface spoiler dee ections for a range of conditions near those for the oscillation cases. The aeroelastic test cases include three types of e utter instability and dynamic response measurements for oscillations of the controls on the e exible mount.