This chapter reviews circulation control wing implementation and integration with the RMRC Anaconda platform. It describes the key elements of the platform and the parameters of the aircraft and goes through a detailed Finite Elements Analysis (FEA) of the CCW.
CITATION STYLE
Kanistras, K., Valavanis, K. P., & Rutherford, M. J. (2018). UC 2 AV: Unmanned Circulation Control Aerial Vehicle. In Intelligent Systems, Control and Automation: Science and Engineering (Vol. 91, pp. 79–97). Springer Netherlands. https://doi.org/10.1007/978-3-319-67852-8_9
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