Verification and Validation Data for Computational Unsteady AerodynamicsComputational Unsteady Aerodynamics computer codes are being increasingly used. In order to validate their results they must be tested against valid experimental data. The present report aims at collecting reliable experimental data on unsteady aerodynamics and presenting them in a form which permits use for verification of codes. For ease of handling, the data are also presented in machine readable form (CD-ROM). Data on increasingly complex generic forms were selected and the following categories are covered: flutter, buffet, stability and control, dynamic stall, cavity flows, store separation. Computational solutions are included in order to permit evaluation of codes and analysis of solutions which differ from experimental data.
IDRelationTitle20010009846Work7E. Test Cases for Flutter of the Benchmark Models Rectangular Wings on the Pitch and Plunge Apparatus20010009849Work9E. Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations20010009847Work8E. Test Cases for the Benchmark Active Controls Model: Spoiler and Control Surface Oscillations and Flutter20010009864Work22-E. Dynamic Data for 2-D and 3-D Test Cases20010009848Work8C. Benchmark Active Controls Technology (BACT) Wing CFD Results20010009845Work6E. Test Cases for a Rectangular Supercritical Wing Undergoing Pitching Oscillations20010009857Work16C. Large-Amplitude, High-Rate Roll Oscillations of a 65° Delta Wing at High Incidence20010009845Work6E. Test Cases for a Rectangular Supercritical Wing Undergoing Pitching Oscillations20010009846Work7E. Test Cases for Flutter of the Benchmark Models Rectangular Wings on the Pitch and Plunge Apparatus20010009847Work8E. Test Cases for the Benchmark Active Controls Model: Spoiler and Control Surface Oscillations and Flutter20010009848Work8C. Benchmark Active Controls Technology (BACT) Wing CFD Results20010009849Work9E. Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations20010009857Work16C. Large-Amplitude, High-Rate Roll Oscillations of a 65° Delta Wing at High Incidence20010009864Work22-E. Dynamic Data for 2-D and 3-D Test Cases