UWS-4 Aero Design: Part 11d, Wing Chordwise Lift Distribution скачать в хорошем качестве

UWS-4 Aero Design: Part 11d, Wing Chordwise Lift Distribution

The chordwise distribution of the pressure (lift) is a large part of what determines the design of the ribs of an airplane. In this video will will talk about chordwise distribution of lift/pressure and then use an estimation method to calculate from Chris Heintz book "Flying on your own wings" to calculate the distribution. 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/ Music: https://www.bensound.com 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.