In this paper the aerodynamic stability of a flat-plate solar tracker under two-dimensional conditions is studied for different conditions of incident wind speed, U∞, nominal angle of attack, αn∈−40∘,40∘, and shaft height - chord ratio H/B=0.3,0.4,0.5,0.6,1and2. The stability is studied through the analysis of the aerodynamic derivatives A2∗ and A3∗ whose behaviours as a function of U∞ are presented for the H/B range studied. Two methods of obtaining the derivatives (one in the time domain and the other one in the frequency domain) are presented. A method for calculating the effective damping coefficient of the solar tracker, ξeff, as a function of the incident wind speed, U∞, is presented. This method can be used for any solar tracker structural characteristics (Jmech, Cmech and Kmech). With this method, the critical speed, Ucrit, can be determined by imposing the condition ξeff=0. The method was validated experimentally using the results of two different experimental set-ups.
CITATION STYLE
Cárdenas-Rondón, J. A., Ogueta-Gutiérrez, M., Franchini, S., & Manzanares-Bercial, R. (2023). Stability analysis of two-dimensional flat solar trackers using aerodynamic derivatives at different heights above ground. Journal of Wind Engineering and Industrial Aerodynamics, 243. https://doi.org/10.1016/j.jweia.2023.105606
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