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Lets determine the geometry for the tail of the UWS-4 Ultralight Airplane. In this, the second part of the tail design, we figure out the shape of the tail, placement of the tail behind the airplane, the surface area, span, chord and control surface chord. We want the place the tail so that it still effective in a stall. Also we don't want a tail strike when we land with a high AoA. Also, in the fist part of this video we decided keep the tail out of the propeller wade. We can use these restrictions to figure out where to place the tail and it helps to determine the shape of the tail. If you want to find more detailed information about the design process you can get Dan's book here (This is an Amazon Associates link which means that the channel will get a small portion of the sale): Dan Raymer's Book "Simplified Aircraft Design for Homebuilders": https://amzn.to/3owAUJL A list of books that I use in my ultralight design efforts can be found here: https://www.ultralightairplaneworksho... If you want to check out the Ultralight Airplane Channel Discord server then here is an invite: / discord If you would like to become a Patron and become an active member on Discord then you can checkout the other perks too here: / ultralight_airplane_workshop 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... 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.