The design report
The design report
The design report
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TRANSLATE<br />
-0.450 0.384 0.00<br />
#<br />
BFIL<br />
fuse.dat<br />
#=============================================<br />
Appendix B – Airfoil Data<br />
NACA4415 - Re = 250000<br />
Alfa Cl Cd Cl/Cd Cm<br />
-3 0.1515 0.0125 12.12 -0.105<br />
-2.5 0.2064 0.0121 17.058 -0.104<br />
-2 0.2605 0.0117 22.265 -0.104<br />
-1.5 0.314 0.0113 27.788 -0.103<br />
-1 0.3651 0.0107 34.122 -0.102<br />
-0.5 0.4121 0.0102 40.402 -0.099<br />
0 0.46 0.01 46 -0.096<br />
1 0.633 0.0104 60.865 -0.108<br />
1.5 0.677 0.0106 63.868 -0.106<br />
2 0.7228 0.0109 66.312 -0.104<br />
3 0.8172 0.0116 70.448 -0.1<br />
3.5 0.8647 0.012 72.058 -0.098<br />
4 0.9127 0.0123 74.203 -0.097<br />
4.5 0.9607 0.0127 75.646 -0.095<br />
5 1.0087 0.0132 76.417 -0.094<br />
5.5 1.0544 0.0136 77.529 -0.092<br />
6 1.0976 0.014 78.4 -0.09<br />
6.5 1.1411 0.0145 78.697 -0.087<br />
7 1.1835 0.015 78.9 -0.085<br />
7.5 1.2223 0.0156 78.353 -0.082<br />
8 1.2564 0.0162 77.556 -0.078<br />
8.5 1.2856 0.0171 75.181 -0.074<br />
9 1.3159 0.018 73.106 -0.07<br />
9.5 1.3408 0.0191 70.199 -0.066<br />
10 1.3594 0.0207 65.672 -0.061<br />
10.5 1.3669 0.023 59.43 -0.055<br />
11 1.3715 0.0257 53.366 -0.049<br />
11.5 1.3662 0.0292 46.788 -0.044<br />
12 1.3513 0.0338 39.979 -0.039<br />
WORTMANN FX 77-W-153 - Re = 250000<br />
Alfa Cl Cd Cl/Cd Cm<br />
-3 -0.052 0.0192 -2.682 -0.024<br />
-2.5 -2E-04 0.0181 -0.011 -0.023<br />
-2 0.052 0.0175 2.9714 -0.022<br />
-1.5 0.1044 0.0169 6.1775 -0.021<br />
-1 0.1587 0.0166 9.5602 -0.02<br />
-0.5 0.206 0.0154 13.377 -0.019<br />
0 0.3244 0.0143 22.685 -0.03<br />
0.5 0.4363 0.0147 29.68 -0.042<br />
1 0.4978 0.0152 32.75 -0.043<br />
1.5 0.5489 0.0155 35.413 -0.043<br />
2 0.5999 0.0159 37.73 -0.042<br />
2.5 0.6508 0.0163 39.926 -0.041<br />
3 0.702 0.0167 42.036 -0.04<br />
3.5 0.7524 0.0174 43.241 -0.04<br />
4 0.8019 0.0178 45.051 -0.039<br />
4.5 0.8519 0.0181 47.066 -0.038<br />
5 0.9028 0.0185 48.8 -0.037<br />
5.5 0.9523 0.0194 49.088 -0.037<br />
6 0.9994 0.0199 50.221 -0.035<br />
6.5 1.0481 0.0204 51.378 -0.035<br />
7 1.0993 0.0207 53.106 -0.034<br />
7.5 1.1456 0.0215 53.284 -0.033<br />
8 1.1903 0.0221 53.86 -0.031<br />
8.5 1.2401 0.0223 55.61 -0.031<br />
9 1.2884 0.0228 56.509 -0.03<br />
9.5 1.3289 0.0229 58.031 -0.028<br />
10 1.3818 0.0225 61.413 -0.027<br />
10.5 1.4143 0.0233 60.7 -0.024<br />
11 1.4593 0.0232 62.901 -0.023<br />
11.5 1.4931 0.0238 62.735 -0.02<br />
12 1.5314 0.0236 64.89 -0.018<br />
12.5 1.5581 0.0242 64.384 -0.015<br />
13 1.5799 0.0247 63.964 -0.011
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