Oscillating 65 Deg. Delta Wing, Experimental

This data set contains force and pressure data resulting from static and dynamic measurements on a sharp-edged cropped delta wing with a leading edge sweep of 65 oscillating in different modes. Motivation for the experiment were the provision of experimental data for validation of unsteady computational codes and understanding of the flow past an oscillating delta wing. The model geometry is identical to a geometry used in the Vortex Flow Experiment for Computer Code Validation VFE, a multinational cooperation which provided experimental data of delta wing configurations in the mid eighties 3, 4 The geometry of the wing is also used for steady and unsteady calculations within the Western European Armament Group WEAG, formerly lEP3TA- ii.