Wind loading on exposed members... Just use Cd = 2! Why waste your time.
If you really want to get technical, drag coefficients are basically characterized by:
1. Flow: Laminar or Turbulent
2. Form: Sharp edged or rounded
3. Longitudinal Length: Long or short
4. Shielding
The first two are intertwined. Sharp edged objects almost always have turbulent flow, rounded objects can be laminar at low fluid velocities (however for structual engineering ultimate wind will be turbulent). A circular (infinitely long) section will have Cd = 1.2 in laminar flow and Cd = 0.4 in turbulent flow when the boundary layer transitions. A long object will always have a high drag coefficient than a short one (out of plane to wind direction), as the fluid can't shed out of plane around the object. Then there's shielding; if the flow has become turbulent or somewhat disturbed before reaching the member in question, ascertaining a drag coefficient other than a conservative guess is futile. Basically it's too complex to waste your time with, and you should increase your beam size if you're concerned.