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Airfoil Investigation (changing angle of attack) |
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July 17, 2014, 15:39 |
Airfoil Investigation (changing angle of attack)
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#1 |
New Member
Dustin
Join Date: May 2014
Posts: 11
Rep Power: 12 |
Hello,
Over the past weeks, I have made decent meshes for different airfoils using ICEM and the simulations have been yielding good results (compared to experimental values). Up until now I have been manually changing the velocity components of the inlet flow to change the angle of attack which is rather time consuming. I now have to repeat this process many times for many different airfoils, and I was wondering if there were more efficient ways to go about this. I can think of some ways but I do not know if they are possible in ANSYS CFX -run one transient simulation where the angle of attach varies and record the forces on the airfoil at defined angles. -predefine all the velocities (like as txt file) and have ANSYS read in the velocities (kind of like a script file) and simulate all velocities in one run If anyone has any experience in this area, I would greatly appreciate your advice and comments. Thank you. |
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July 17, 2014, 19:16 |
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#2 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,870
Rep Power: 144 |
You can do this in workbench using parameters. Alternately you can also do this with different CCL files and script them all together.
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July 22, 2014, 03:52 |
Thrust Problem
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#3 |
New Member
M Mohsin Iqbal
Join Date: Jan 2014
Location: National University Sciencies & Technology, Pakistan
Posts: 17
Rep Power: 12 |
Hi Sir
Hope so you will be fine and good. Sir i have a question regarding thrust of a propeller. Why Thrust of a propeller decreases with increase in Advanve Ratio??? Similarly Torque of Propeller ??? only propeller thrust and torque without engine. Thanks Looking Forward |
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