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byuflowlab / FLOWUnsteady

An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy
https://flow.byu.edu/FLOWUnsteady/
MIT License
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How to obtain variable parameters? #191

Open Liuhaosheng1 opened 2 months ago

Liuhaosheng1 commented 2 months ago

Hello author,

You wrote about wheel hub correction in section 6.2.1 of your doctoral thesis, which mentioned the wheel hub correction equation, followed by variable parameters t1, t2, t3, h1, h2, and h3. You explained the meanings of other characters and how to obtain numerical values in your paper, but did not mention how variable parameters are obtained. If one wants to create a new airfoil, how should these variable parameters be defined or valued, and what is the basis for their numerical values? I believe this is a question that scientific research needs to consider. And in the case of wheel hub correction mentioned in your paper, you did not explain the basis for the values, and if the adjustable parameters in your case were modified, the comparison between the results obtained and the experiment would be much worse.

I have conducted multiple simulations, but have not yet come up with the basis for the variable parameters. I have to ask the author if they can give me an answer

Thank you very much.

Best wishes

sakurakikiki commented 1 week ago

Did you get the right answer?