Experimental investigation of the pressure distribution about a yawed circular cylinder in the critical Reynolds number range

Report presenting an experimental investigation of the pressure distribution about a circular cylinder at yaw angles of 0, 15, 30, 45, and 60 degrees and a variety of Reynolds numbers. Testing indicated that for the range of Reynolds number near and above the critical value, the flow and force characteristics of a yawed circular cylinder cannot be determined only by the component of flow normal to the axis of the cylinder.