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 upper-surface spoiler oscillations for a range of Mach numbers, angle of attack, and static control deflections are included. Cases also include static angles of attack, static trailing-edge control, and static upper-surface spoiler deflections for a range of conditions near those for the oscillation cases. The aeroelastic test cases include three types of flutter instability and dynamic response measurements for oscillations of the controls on the flexible mount. (Author)