Finding the drag and lift coefficients at any given location

Djphx · January 9, 2019, 05:25

Hi,
I am simulating a flow around a 3d circular cylinder. I know how to obtain the cd and cl values with time for a transient model but am unaware of how to get the cd and cl values at each location (spanwise/ lengthwise). Please help.

Thanks in advance

LuckyTran · January 9, 2019, 17:21

Cd and Cl are integrated properties and do not exist locally. What you are looking for is not Cd and Cl. So you need to clarify.....

Djphx · January 10, 2019, 00:45

Hi,
Is there a way to get the cd and cl values integrated over a fixed length of area (like cd and cl values integrated over the location/total length ratio of 0 to 0.1 and 0.1 to 0.2 and so on)?

January 9, 2019, 05:25	Finding the drag and lift coefficients at any given location	#1
Djphx New Member Djphoenix Join Date: Oct 2018 Posts: 7 Rep Power: 7	Hi, I am simulating a flow around a 3d circular cylinder. I know how to obtain the cd and cl values with time for a transient model but am unaware of how to get the cd and cl values at each location (spanwise/ lengthwise). Please help. Thanks in advance

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January 9, 2019, 17:21		#2
LuckyTran Senior Member Lucky Join Date: Apr 2011 Location: Orlando, FL USA Posts: 5,739 Rep Power: 66	Cd and Cl are integrated properties and do not exist locally. What you are looking for is not Cd and Cl. So you need to clarify.....

January 10, 2019, 00:45		#3
Djphx New Member Djphoenix Join Date: Oct 2018 Posts: 7 Rep Power: 7	Hi, Is there a way to get the cd and cl values integrated over a fixed length of area (like cd and cl values integrated over the location/total length ratio of 0 to 0.1 and 0.1 to 0.2 and so on)?