Computational test cases for the benchmark active controls model

Unsteady aerodynamic and aeroelastic computational test cases have been sel ected 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 sta tic control deflections are included. Cases also include static angles of a ttack, static trailing-edge control, and static upper-surface spoiler defle ctions for a range of conditions near those for the oscillation cases. The aeroelastic test casts include three types of flutter instability and dynam ic response measurements for oscillations of the controls on the flexible m ount.