Drag Coefficient (Cd) values for I-beams, Channels, etc.

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Discussion Overview

The discussion revolves around the determination of drag coefficient (Cd) values for I-beams and similar structural shapes under various flow orientations. Participants seek to clarify the appropriate Cd values for flow parallel to the I-beam, as well as for flow impacting the web and flat plate areas of the beam.

Discussion Character

  • Technical explanation
  • Debate/contested
  • Mathematical reasoning

Main Points Raised

  • One participant requests Cd values for I-beams, specifically for flow parallel to the beam and from the top and side, noting a previously found value of 2.7 without clarification on orientation.
  • Another participant suggests that the 2.7 value likely pertains to flow perpendicular to the beam's length and questions the clarity of the original request.
  • A different participant expresses skepticism about the 2.7 value, comparing it to the drag coefficients of parachutes, which are lower.
  • One participant proposes using Cd values of 1.6 for flow onto the web and flat plate areas, while suggesting that the Cd for flow parallel to the web would be low but still significant due to the end face drag factor.
  • There is a discussion about whether the Cd value for flow onto the web (Cd1) would be higher than that for the flat plate (Cd2), with some participants indicating that the projected area is used for wind force calculations.
  • Another participant notes that airflow hitting the web side would be restricted by the plates, potentially leading to a higher Cd value for that orientation.
  • A participant shares links to images that helped clarify their confusion and mentions finding a PDF with relevant drag coefficient information for hollow sections.

Areas of Agreement / Disagreement

Participants express differing views on the appropriate Cd values for various orientations, with no consensus reached on the exact values or their implications. The discussion remains unresolved regarding the specific Cd values for the different flow conditions.

Contextual Notes

Participants reference various assumptions about flow orientation and projected areas, but these assumptions are not universally agreed upon. The discussion includes uncertainty regarding the accuracy of the Cd values mentioned and their applicability to different scenarios.

HoBBLeCooKiE
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Can anyone PLEASE help me in pointing me in the right direction? I need to obtain drag coefficient calues for I-beams. I found a site stating it was 2.7, but it says nothing about the orientation?? I basically need the Cd-value for flow parallel to the I-beam, from the top and from the side.

Any help will be appreciated.

Thanks!
 
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I think you need to clarify your request. Your use of the word parallel and then "from the top and bottom" seems in conflict. The 2.7 number is likely for a flow perpendicular to the length and sounds pretty reasonable.
DC
 
Last edited:
2.7 sounds really high. A very good parachute has a cd of about 2.2-2.5.
 
DarioC said:
I think you need to clarify your request. Your use of the word parallel and then "from the top and bottom" seems in conflict. The 2.7 number is likely for a flow perpendicular to the length and sounds pretty reasonable.
DC

What I meant was that I need 3 Cd values. (I attached a quick sketch of it.)

[PLAIN]http://img32.imageshack.us/img32/6361/ibeam.jpg

Cd values are for:

1 - Flow onto "web" area.
2 - Flow onto flat "plate" area.
3 - Flow parallel to the length of the I-beam.

I would like to see the change in wind load according to change in orientation.
 
Last edited by a moderator:
I would use Cd1 and Cd2 as 1.6. For Cd3, I've never used it, but I assume it's value would be very low parallel to the web, and dwarfed by the drag factor on the end face, which would again be about 1.6.
 
PhanthomJay said:
I would use Cd1 and Cd2 as 1.6. For Cd3, I've never used it, but I assume it's value would be very low parallel to the web, and dwarfed by the drag factor on the end face, which would again be about 1.6.

Wouldn't the value for Cd1 be a bit higher than Cd2?
 
HoBBLeCooKiE said:
Wouldn't the value for Cd1 be a bit higher than Cd2?
Perhaps, but I've aways in both cases just used the projected area to calculate the wind force, using the drag factor for a 'flat' surface (Cd = 1.0 for a cylindrical face, Cd =1.6 for a flat face).
 
PhanthomJay said:
Perhaps, but I've aways in both cases just used the projected area to calculate the wind force, using the drag factor for a 'flat' surface (Cd = 1.0 for a cylindrical face, Cd =1.6 for a flat face).

Yes, but when the air hits the web side (as in Cd1) it will be restricted when trying to move around the web area because of the plates either side. This will definitely cause the Cd value to be higher.
 

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