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Liusst December 14, 2016 08:37

I really need your help!!
 
4 Attachment(s)
Hello everyone! I try to do a research of conjugate heat transfer, and I use MARKⅡturbine blade for that. Now I have the coordinates of blade and blade's holes(like picture 1 and picture 2), but when I put into ICEM, It is like picture3,how can I do that they can like picture 4? How should I do to transform for that? I really need your help! Thanks in adcance!:D:D

dscian December 18, 2016 11:40

Hi,

I can help you with that.

Utkan

Liusst December 18, 2016 19:58

Quote:

Originally Posted by dscian (Post 630226)
Hi,

I can help you with that.

Utkan

Thank you for your reply! Can you tell me how to do that? How to get the hole's coordinate in the same axis? I'm carzy now!:eek::confused:

Liusst December 19, 2016 10:57

Quote:

Originally Posted by dscian (Post 630226)
Hi,

I can help you with that.

Utkan

can you tell me how to do that?:confused::confused::confused:

topspin247 December 20, 2016 09:10

Can you try this link:

https://www.cfd-online.com/Forums/an...-blocking.html

Liusst December 20, 2016 11:03

Quote:

Originally Posted by topspin247 (Post 630578)

thank you for you reply! but this is not the answer I want, I just wonder how to change the holes coordinates that the model like picture4.:confused:

topspin247 December 20, 2016 11:44

If you know the angle between picture 3 and picture 4, you can do a rotation on all of the data points for the geometry to manually rotate it BEFORE importing into ICEM. That to me is the quickest way and can be done easily in excel, MATLAB, python, etc.

Liusst December 21, 2016 06:56

Quote:

Originally Posted by topspin247 (Post 630599)
If you know the angle between picture 3 and picture 4, you can do a rotation on all of the data points for the geometry to manually rotate it BEFORE importing into ICEM. That to me is the quickest way and can be done easily in excel, MATLAB, python, etc.

Hi
Thank you for your reply! I have tried to do a ratation on holes coordinates in Excel before I ask for help, but I failed, the following is what I have done. Just like picture 1, I know the setting angle is 63deg41min31sec, so I use the following formula to convert:
x=(x1-x0)cosa-(y1-y0)sina+x0
y=(x1-x0)sina+(y1-y0)cosa+y0
where (x1,y1) is holes coordinates, (x,y) is holes coordinates after rotation, (x0,y0) I am not sure how to choose, I use the point (3.434, 6.909) in picture1.
It is wrong with my formula?
Point datas are from this article 《analytical and experimental evaluation of the heat transfer distribution over the surfaces of turbine vanes》page 11-16. Can you help me for that? I'm quite new.....

topspin247 December 21, 2016 09:24

Quote:

Originally Posted by Liusst (Post 630763)
Hi
Thank you for your reply! I have tried to do a ratation on holes coordinates in Excel before I ask for help, but I failed, the following is what I have done. Just like picture 1, I know the setting angle is 63deg41min31sec, so I use the following formula to convert:
x=(x1-x0)cosa-(y1-y0)sina+x0
y=(x1-x0)sina+(y1-y0)cosa+y0
where (x1,y1) is holes coordinates, (x,y) is holes coordinates after rotation, (x0,y0) I am not sure how to choose, I use the point (3.434, 6.909) in picture1.
It is wrong with my formula?
Point datas are from this article 《analytical and experimental evaluation of the heat transfer distribution over the surfaces of turbine vanes》page 11-16. Can you help me for that? I'm quite new.....

Use the following equation for rotating about the origin, where x and y are the current points and x' and y' are the rotated point:

https://www.cfd-online.com/Forums/da...AAAElFTkSuQmCChttp://i.imgur.com/tLiKn1U.png

I think in your equation, (x0,y0) is the point of rotation (if it's not the origin).

sources:
https://www.siggraph.org/education/m...ran/2drota.htm
https://en.wikipedia.org/wiki/Rotation_(mathematics)


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