WindData - Drag Force vs. Strain 8.00E-01 f(x) = -7619.21x...

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0.43 0.43 0.43 0.43 0.43 0.43 0.43 0.43 0.43 0.43 0.43 0.00E+00 1.00E-01 2.00E-01 3.00E-01 4.00E-01 5.00E-01 6.00E-01 7.00E-01 8.00E-01 f(x) = -7619.21x + 3307.4 R² = 0.97 Drag Force vs. Strain Strain Drag Force (N)
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7.00E+03 9.00E+03 1.10E+04 1.30E+04 1.50E+04 1.70E+04 1.90E+04 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 1.1 1.2 1.3 1.4 1.5 1.6 Reynolds number vs. Drag Column H Column G Column R Column R Reynolds number Drag Coefficient
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Airfoil Trial Temp Strain Pressure differential Fd U 1 22.36 0.43 -1.71 -0.28 1.71 2 22.36 0.43 72.09 -0.15 11.08 3 22.35 0.43 122.54 -0.1 14.45 4 22.34 0.43 181.14 0 17.57 5 22.31 0.43 223.49 0.06 19.52 6 22.31 0.43 231.72 0.07 19.87 7 22.27 0.43 284.31 0.13 22.01 Avg. Temp. 22.33 Density 1.17 Cylinder Trial Temp Strain Pressure differential Air Velocity Re Cd 1 22.25 0.43 -1.47 #VALUE! #VALUE! 0.00E+00 2 22.19 0.43 65.01 10.53 8.76E+03 1.10E+00 3 22.31 0.43 110.98 13.75 1.15E+04 1.10E+00 4 22.27 0.43 158.35 16.43 1.37E+04 1.10E+00
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This note was uploaded on 06/15/2009 for the course MAE 3183 taught by Professor Staff during the Spring '08 term at UT Arlington.

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WindData - Drag Force vs. Strain 8.00E-01 f(x) = -7619.21x...

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