HI im doing a science project in school . we want to study different type of wingtip on wing's effect ,so can i ask you that how did you made the wing model in openfoam please? do u have a video about it ?
Which tutorial describes the setup in detail? It sounded like you said "rotating fan in room", but I don't see anything like that on your TH-cam channel page.
I was referring to a tutorial case in openfoam, you can find more here: www.openfoam.com/documentation/guides/latest/doc/tutorial-pimplefoam-ami-rotating-fan.html and a video on it here: th-cam.com/video/qtN256WJ-5I/w-d-xo.html
Very nice tutorial. I am running a simular case with an off-shore turbine, my dynamic mesh seems to work but my setup is a such a mess. May I contact you for some advice? Cheers!
I agree CL/CD of 4 is too low. This is clearly as a result of methods used. I have found similar results (~3.5)in OpenFOAM for a wing I have tested in reality and found to be about 20. Does anyone know why the value is so low?
HI im doing a science project in school . we want to study different type of wingtip on wing's effect ,so can i ask you that how did you made the wing model in openfoam please? do u have a video about it ?
Nice video. love to see a ground effects wing with dynamic mesh.
Which tutorial describes the setup in detail? It sounded like you said "rotating fan in room", but I don't see anything like that on your TH-cam channel page.
I was referring to a tutorial case in openfoam, you can find more here: www.openfoam.com/documentation/guides/latest/doc/tutorial-pimplefoam-ami-rotating-fan.html
and a video on it here: th-cam.com/video/qtN256WJ-5I/w-d-xo.html
Very nice tutorial. I am running a simular case with an off-shore turbine, my dynamic mesh seems to work but my setup is a such a mess. May I contact you for some advice? Cheers!
nice video sir.......can you help me .......to simulate RANS in openfoam ...... i have...... generated 3dwing mesh in icem cfd and imported here.....
CL/CD of less than 4 is very weird at this Reynolds number
I agree CL/CD of 4 is too low. This is clearly as a result of methods used. I have found similar results (~3.5)in OpenFOAM for a wing I have tested in reality and found to be about 20. Does anyone know why the value is so low?
Very nice. p.s. i kometarze w SolidWorks po polsku. Pozdrowienia ;)
greetings