Computational Test Cases for the Benchmark Active Controls Model

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.