The Compendium is intended to assist the development of improve d methods of predicting transonic unsteady aerodynamics and aeroelastic response by collecting the known unsteady aerodynamic experimental data for the standard AGARD two-dimensional and three-dimensional aeroelastic configurations published in AGARD Advisory Reports 156 and 167 respectively. This Report was sponsored by the Structures and Materials Panel of AGARD. (Author)


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