This website provides information on our Aeroelastic Sensing project. In this project, a wind-tunnel model was designed and printed using rapid prototyping. The wing was tested in the subsonic wind tunnel of the Faculty of Aerospace Engineering, Technion, at various airspeeds and all the way to flutter. Data collected includes accelerations and strains from uni-axial strain gauges and strains from optical fibers. This webpage was put together in order to share the models, experimental data, and publications, with the aeroelasticity research community. The website is under construction and so is the Aeroelastic Sensing project. Please feel free to contact us for more data or information, or any questions regarding the project and models. With time we hope to improve the data in this webpage and make it valuable to the aeroelasticity community.