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used this tutorial to help validate my CFD results for uni, flaps part was especially helpful as i had no other way to validate them! Many thanks!
Is there a non manual way to change the text file format? Like a C code or something.
Very very impressive!
very nice video, thank you
What is the CDp column?
drag coefficient , consists of 2 components: the cdf , due to friction and viscous phenomena and cdp (the one you are referring to) , which is the drag caused by the shape of the airfoil (it exists and in non viscous flows)
yo´re the best, thnak U very much
How to export cp graph to excel file from xfoil?
There's a command in XFOIL called CPWR with allows you to write your x vs Cp values to a file
@@spaceshuttle8332 Working. Thanks ya
Thank you
Thank you 🙏
used this tutorial to help validate my CFD results for uni, flaps part was especially helpful as i had no other way to validate them! Many thanks!
Is there a non manual way to change the text file format? Like a C code or something.
Very very impressive!
very nice video, thank you
What is the CDp column?
drag coefficient , consists of 2 components: the cdf , due to friction and viscous phenomena and cdp (the one you are referring to) , which is the drag caused by the shape of the airfoil (it exists and in non viscous flows)
yo´re the best, thnak U very much
How to export cp graph to excel file from xfoil?
There's a command in XFOIL called CPWR with allows you to write your x vs Cp values to a file
@@spaceshuttle8332 Working. Thanks ya
Thank you
Thank you 🙏