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Designing an airplane is an iterative process. We have been through the initial aerodynamic design of the UWS-4 Ultralight airplane and now it is time to start the first iteration of the aerodynamic analysis. In this video we will determine a more accurate estimation of the Coefficient of Parasitic Drag, Coefficient of Induced Drag and the Coefficient of maximum lift of the wing. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" https://www.ultralightairplaneworksho... Links: Youtube Channel: / @designer103 Patreon: / ultralight_airplane_workshop Facebook: / ultralightairplaneworkshop Twitter: / designer1032 Website: https://www.UltralightAirplaneWorksho... FAA AC 103-7: https://www.faa.gov/documentLibrary/m... Xflr5 software: OpenVSP: http://openvsp.org/ Disclaimer: If you use any of the information that you see on this video on a project of your own, YOU become the engineer and responsible party for your project. It is possible that miscalculations were made in the production of this video. Since you are now the engineer for your project, you must verify the information that you use.