You are conducting a wind tunnel test to measure the aerodynamic drag ("air resistance") over a...
. max A small round object is tested in a 0.75-m diameter wind tunnel. The pressure is uniform across sections 1 and 2. The upstream pressure is 30 mm H2O (gage), the downstream pressure is 15 mm H20 (gage), and the mean air speed is 12.5 m/s. The velocity profile at section 2 is linear; it varies from zero at the tunnel centerline to a maximum at the tunnel wall. V Calculate a) the mass flow rate in the wind...
An engineer is measuring the lift and drag on an aerofoil section mounted in a square wind tunnel. The wind tunnel is 0.5 m high and 0.5 m deep into the screen). The upstream air velocity is uniform at 25 m/s. The downstream velocity is uniform at 28.75 m/s in the lower half of the wind tunnel. The downstream velocity in the upper half is uniform. The vertical component of velocity is zero at the beginning and end of the...
1. Measuring Drag on a Cylinder Pre-Lab Analysis: You will test two free-stream velocities of 10 and 20 m/s and two cylinder diameters of 19 mm and 38 mm, depending on which wind tunnel you use. In preparation for the lab calculate the following: a. The expected dynamic pressure values in units of inH20 that you would expect to measure for air moving at 10 m/s and 20 m/s, respectively. Write the calculated values into the "Predicted Pdyn (inH20) from...