Hello.My name is am. this is the first thread that i wrote. i am beginner in using FineHexa. im doing miniproject about WiG aircraft. my objective is just to get the value of lift coefficient and drag coefficient, that all. i already done the meshing, create the box until applying the viscous layer. the problem is, i dont know how to use the fine hexa to run the simulation. i already import the meshing file, and next i dont how to enter the data, which parameter need to be default, which must be fill. Can someone help me please? or have some tutorial regarding to aerodynamic analysis? very need someone help right now.im using FineHexa 2.10.4 right now.
please email me : email@example.com
Running the computation may need some technique and thus you will need to go for some training. From the training, you will know what is the best mesh suit for your computation. The physical parameters that you provide is sensitive to your output (Post-result) and we don't stick to 'rubbish-in-rubbish-out'. You could contact me for more info.
NUMIT Enterprise, Malaysia
+6 017 656 3436
Email : firstname.lastname@example.org
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