High Angle Working Group Analyses in Support of the Third Aeroelastic Prediction Workshop: Flutter Predictions

This paper presents a summary of the computational flutter results associated with the AIAA Third Aeroelastic Prediction Workshop, High Angle Working Group. The computational results are compared against the experimental data collected during the Pitch and Plunge Apparatus Benchmark Supercritical Wing test campaign conducted in the Transonic Dynamics Tunnel at NASA Langley Research Center in 1993. During that test, several flutter points were identified at transonic conditions. One of these poin