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1. |
During test-run, air flows at 215 m/s velocity and 25 degree Celsius temperature past a smooth thin model airfoil which can be idealized as a flat plate. If the chord length of the airfoil is 15 cm, find drag per unit width. The relevant physical properties of air are
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A. | nv = 15.53 * 10 <sup>-6</sup> m<sup>2</sup>/s |
B. | 25.42 N per unit width |
C. | 35.42 N per unit width |
D. | 45.42 N per unit width |
E. | 55.42 N per unit width |
Answer» B. 25.42 N per unit width | |