Hi! If I want to test in ANSYS just a part of the inferior flange of my spar, which has three holes, what boundary conditions (forces, etc...) would you choose? Can you help me, please? Thanks!
there are some coordinates that ansys refuses to plot for that you just jse solid work or catia to do the plotting and surface generation and import it to ansys
This is still an airfoil and not a wing. There is nothing called as a 3D airfoil. When you say 3D airfoil it means wings with no end effects. This will produce tremendous amount of drag if you put end plates. Hence this is not accurate. If you want to simulate wings then you should also simulate the end effects. this is just an airfoil
Hi! If I want to test in ANSYS just a part of the inferior flange of my spar, which has three holes, what boundary conditions (forces, etc...) would you choose? Can you help me, please? Thanks!
Would it give the same results if I started with cfd and used the mesh of cfd in static structural analysis?
Thank you very much
For some reason, the program is not able to read the cordinates, did you put the text format in tabs?
Thanks and help-me 😅
there are some coordinates that ansys refuses to plot for that you just jse solid work or catia to do the plotting and surface generation and import it to ansys
Hi
Please can you do step by step exhaust fan simulation and Fan rotation animation
I would like to do that but my System configuration cannot handle the loads. will do if I upgrade mine
What is the material used in that wing?
By default the material is normally structural steel, so im guessing thats what it is as he hasnt made any changes to it.
7:56
This is still an airfoil and not a wing. There is nothing called as a 3D airfoil. When you say 3D airfoil it means wings with no end effects. This will produce tremendous amount of drag if you put end plates. Hence this is not accurate. If you want to simulate wings then you should also simulate the end effects. this is just an airfoil
Why we should care end effects