UNIVERSIDAD NACIONAL DEL SANTAFACULTAD DE INGENIERIA EN ENERGIA

INGENIERIA DE LA ENERGIA EOLICA

"PROGRAMA PARA PARAMETROS DE UN AEROGENERADOR"

RESPONSABLES:PORTAL JIMENEZ JOSE LUISBADA VALERA HELICHAVEZ ARIAS WILFREBLAS SARSOZA ADOLFO

MENU

Ingreso de Datos ( Mediciones)

LIMPIAR(Ingresar nuevos datos)

IMPRIMIR

UNIVERSIDAD NACIONAL DEL SANTA

"PROGRAMA PARA PARAMETROS DE UN

MENU

Ingreso de Datos ( Mediciones)

LIMPIAR(Ingresar nuevos datos)

IMPRIMIR

PERFILES DE VELOCIDAD DEL VIENTO (m/s), ZONA POSTERIOR DE LA FACULTAD DE EDUCACION DE LA UNS,(16 DE ENERO - 11 DE FEBRERO - 2006

D I A S1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21

m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s7:00 0.00 0.06 0.00 1.51 1.02 0.00 0.00 2.61 0.00 0.90 1.02 0.00 2.89 1.97 0.00 1.68 0.00 0.00 1.27 0.42 2.497:10 0.00 0.02 0.00 2.63 1.51 0.00 0.00 2.08 0.00 0.69 1.51 0.00 3.41 1.92 0.00 0.59 0.00 0.00 1.96 0.87 2.137:20 0.00 0.14 0.00 0.04 2.36 0.00 0.00 3.14 0.00 1.10 2.36 0.00 0.84 1.91 0.00 0.17 0.00 0.00 2.56 1.01 3.067:30 0.00 0.18 0.00 0.45 0.98 0.00 0.00 4.44 0.00 1.13 0.98 0.00 0.41 2.15 3.29 0.70 0.00 0.00 1.72 2.38 3.237:40 0.00 0.41 2.95 2.83 0.86 4.67 2.14 4.89 1.93 0.74 0.86 0.00 2.67 2.10 3.02 3.12 0.00 0.00 1.03 1.89 2.957:50 0.28 0.30 3.02 2.03 1.96 4.12 0.94 4.77 1.81 3.42 1.96 0.00 1.93 2.62 3.09 1.13 0.00 0.00 2.66 1.97 3.028:00 1.13 0.57 2.41 1.42 2.65 3.92 2.28 5.46 2.05 1.39 2.65 0.00 3.18 3.26 2.47 1.41 0.53 0.00 1.86 2.71 2.418:10 0.54 0.19 2.82 3.24 2.49 2.70 3.54 5.01 2.22 1.59 2.49 0.00 2.35 3.41 2.89 3.11 0.33 0.00 1.11 2.58 2.828:20 1.92 0.41 3.20 1.60 2.08 4.96 4.50 4.03 2.67 3.15 2.08 0.00 1.45 2.62 3.26 1.56 0.61 0.00 2.54 3.26 3.208:30 0.63 0.29 3.30 4.46 3.75 5.91 2.73 3.26 3.01 2.27 3.75 0.00 1.51 3.71 3.37 4.98 0.00 0.42 2.63 1.85 3.308:40 0.97 0.69 4.01 3.73 2.57 7.33 4.35 4.64 3.38 3.68 2.57 0.00 4.04 3.92 4.08 2.96 0.94 0.00 3.33 3.41 4.018:50 0.01 0.98 3.35 3.99 2.32 4.38 5.50 5.25 2.93 3.38 2.32 0.00 3.41 3.57 3.41 2.19 1.31 0.87 3.06 2.55 3.359:00 1.94 1.39 2.49 3.88 3.38 3.40 4.25 5.66 2.96 2.12 3.38 3.60 3.80 4.40 3.64 1.49 1.59 1.18 2.30 4.04 2.499:10 3.84 1.71 3.84 0.43 1.96 2.85 4.81 5.34 2.78 0.81 1.96 3.77 1.11 4.83 3.91 1.49 2.12 1.09 1.35 3.74 2.519:20 3.55 0.86 2.67 3.54 2.53 4.40 4.68 5.87 3.18 0.90 2.53 3.82 2.42 4.12 2.73 5.22 1.02 2.05 2.45 3.54 2.309:30 2.43 1.35 3.41 1.44 3.06 2.59 4.33 5.46 2.66 2.53 3.06 3.98 2.02 4.21 3.48 2.13 1.26 3.95 1.96 4.43 2.429:40 2.79 2.08 2.46 4.24 3.87 3.04 4.05 6.15 3.22 3.63 3.87 4.69 2.13 4.05 2.52 2.99 0.00 2.01 2.43 4.68 2.239:50 1.64 1.71 2.93 4.58 3.42 4.87 2.89 3.16 3.15 5.62 3.42 7.18 2.80 4.66 2.99 4.54 1.22 4.16 2.85 4.58 3.79

10:00 4.68 2.85 2.42 4.43 2.16 4.99 2.90 5.24 3.49 4.29 2.16 4.03 0.00 4.38 2.53 3.82 0.94 3.83 3.57 4.31 4.1210:10 3.30 2.61 3.24 4.19 4.40 5.04 2.18 3.83 3.57 4.17 4.40 3.11 2.21 2.79 3.35 4.12 1.26 2.78 5.13 2.64 3.3610:20 4.90 2.00 2.33 4.00 3.54 5.19 6.05 5.08 4.00 2.59 3.54 2.24 1.21 2.95 2.44 1.45 1.39 3.76 5.66 2.86 4.3310:30 3.18 2.89 4.38 3.32 3.10 2.87 4.21 5.38 3.42 3.40 3.10 4.17 0.23 6.30 4.49 5.40 0.65 3.62 3.83 6.33 3.87

10:40 2.56 4.44 3.66 2.86 2.65 4.33 5.80 2.82 3.76 2.20 2.65 4.58 0.23 4.37 3.77 0.71 1.02 5.65 3.69 4.15 4.5510:50 6.78 1.79 3.52 1.61 3.54 6.73 3.09 5.62 3.87 1.48 3.54 4.95 0.00 3.56 3.62 2.26 0.69 4.88 3.94 3.37 4.7311:00 5.34 1.39 3.08 1.80 2.97 6.04 4.53 3.63 3.59 1.29 2.97 5.48 2.34 6.64 3.19 5.73 1.22 7.34 4.43 6.86 4.66

11:10 7.34 1.71 2.47 2.19 1.71 4.00 6.77 4.46 3.74 2.39 1.71 3.66 0.77 5.47 2.58 6.70 2.04 3.78 4.81 5.36 7.0711:20 7.71 2.40 3.46 4.58 2.45 3.46 2.14 7.32 3.74 5.42 2.45 3.51 3.81 7.02 3.56 5.07 0.00 4.08 1.18 7.06 7.1611:30 6.91 2.28 5.20 6.00 2.28 5.58 3.82 6.17 4.58 3.72 2.28 3.11 2.55 5.72 5.31 4.99 0.37 2.45 5.51 7.97 6.6011:40 8.61 1.18 6.69 3.24 1.39 6.95 2.63 7.11 4.39 3.13 1.39 2.65 1.93 4.38 6.80 4.27 0.10 6.51 4.48 4.23 7.0211:50 6.63 2.85 5.82 5.82 5.30 8.25 1.64 6.79 5.19 5.96 5.30 1.81 1.56 7.46 5.92 4.72 0.30 4.22 6.95 5.87 10.6012:00 10.74 3.54 5.54 6.40 2.85 7.34 5.70 5.47 6.02 6.11 2.85 4.07 4.99 7.71 5.64 4.57 0.86 3.99 5.15 5.63 7.4912:10 10.22 3.05 7.26 6.99 6.68 6.39 3.76 7.01 6.34 6.90 6.68 5.04 3.43 7.07 7.36 4.69 0.00 4.51 3.46 5.41 7.67

HORA

12:20 6.46 1.87 6.54 2.38 4.32 5.43 2.47 6.85 4.21 2.13 4.32 5.49 2.76 4.67 6.64 4.13 0.90 5.11 1.57 4.71 10.8312:30 12.03 3.75 7.52 6.89 1.67 8.30 6.40 8.65 6.65 6.92 1.67 5.92 3.97 5.26 7.62 7.79 0.90 4.03 3.61 5.30 9.2012:40 9.29 3.68 7.32 8.74 4.85 7.47 6.08 9.18 6.78 8.81 4.85 4.84 3.87 4.64 7.43 4.34 2.36 4.70 3.88 4.79 9.5312:50 9.92 3.32 6.90 3.66 3.42 9.09 4.48 6.75 5.83 4.50 3.42 5.12 3.93 4.87 7.01 4.58 1.18 5.61 4.77 4.95 8.8013:00 8.04 3.42 7.67 3.57 5.46 9.59 4.67 6.53 6.06 6.07 5.46 7.41 8.22 6.57 7.78 7.49 1.47 5.98 1.50 6.65 9.8213:10 8.34 3.54 8.54 6.50 4.64 7.55 9.53 10.45 6.95 6.65 4.64 6.74 4.45 8.30 8.65 4.86 4.97 8.26 7.15 8.45 9.0813:20 10.31 2.95 11.09 6.31 4.03 7.82 8.32 8.66 7.26 6.52 4.03 5.84 6.71 8.62 11.20 4.25 2.65 4.01 5.71 8.76 9.1613:30 8.74 2.67 14.07 7.71 5.66 7.18 9.16 10.53 7.88 7.90 5.66 7.64 4.96 9.13 14.17 9.42 2.93 8.24 6.51 9.47 11.0013:40 11.19 3.44 9.99 6.91 4.03 6.35 6.57 10.56 6.93 6.77 4.03 8.30 4.68 5.39 10.10 5.71 5.50 5.12 3.60 5.03 10.3013:50 7.85 3.70 7.27 3.61 4.44 6.58 6.88 9.53 5.76 7.51 4.44 7.70 8.02 7.62 7.38 8.41 4.73 4.68 8.05 7.45 10.0614:00 6.64 2.86 9.82 6.82 4.81 7.83 7.93 8.53 6.67 6.86 4.81 6.57 9.04 7.72 9.92 7.92 3.54 7.80 7.63 4.57 10.3014:10 6.18 5.19 11.29 5.04 3.95 6.31 7.51 8.25 6.49 6.80 3.95 9.10 7.02 7.62 11.39 4.12 4.77 7.86 6.86 3.55 11.4214:20 7.16 2.55 7.36 8.15 7.98 7.14 4.76 10.45 6.44 8.17 7.98 7.64 10.59 7.97 7.47 7.54 3.22 8.22 8.19 3.82 7.4914:30 8.96 3.98 7.52 8.10 4.44 9.94 3.10 9.30 7.58 8.13 4.44 9.97 10.06 7.81 7.62 7.52 2.97 5.49 5.79 7.73 7.6514:40 8.40 5.15 7.64 4.14 2.20 10.00 7.60 8.23 7.70 3.71 2.20 9.60 6.22 8.00 7.75 7.90 2.40 9.60 6.38 5.22 7.7814:50 7.65 5.27 7.63 5.69 6.44 7.49 4.06 9.18 7.69 5.78 6.44 9.99 7.67 7.58 7.74 4.67 2.00 8.69 11.66 7.81 7.7615:00 5.85 3.86 7.75 7.48 8.76 6.25 7.97 8.40 7.80 7.67 8.76 7.23 8.82 7.77 7.85 8.42 4.93 5.95 9.92 7.71 7.8815:10 5.78 3.57 4.33 5.92 5.74 9.69 5.35 8.63 4.38 5.54 5.74 6.39 7.84 6.53 4.43 8.46 7.21 8.49 11.24 6.56 4.4615:20 5.79 3.88 5.06 8.24 6.44 7.56 6.40 9.44 5.12 8.43 6.44 9.10 7.95 6.93 5.17 4.56 8.55 10.13 10.35 6.96 5.1915:30 7.07 5.59 5.32 9.60 7.33 10.04 7.70 5.47 5.38 10.08 7.33 4.43 8.85 5.63 5.43 8.51 4.77 9.57 7.56 5.33 5.4515:40 5.94 4.66 5.93 7.58 6.76 5.30 8.60 8.89 5.99 7.82 6.76 9.55 9.81 4.59 6.04 12.66 4.60 6.53 8.08 4.74 6.0715:50 6.21 4.27 7.24 7.51 5.46 6.13 12.14 4.94 7.29 7.07 5.46 7.97 7.31 6.29 7.34 7.18 4.40 9.10 6.76 5.93 7.3716:00 7.71 4.62 7.37 9.75 7.17 5.54 11.05 6.53 7.43 8.68 7.17 7.56 9.62 5.98 7.48 7.98 3.71 11.86 6.46 6.78 7.5016:10 6.91 4.14 7.51 3.59 8.11 4.13 8.68 8.21 7.56 3.22 8.11 5.92 9.96 4.59 7.61 9.07 10.51 8.04 8.92 4.95 7.6416:20 6.86 4.07 6.61 3.03 7.13 6.22 4.46 8.57 6.67 3.46 7.13 6.37 9.38 4.21 6.72 7.45 7.66 10.31 7.29 5.38 6.7516:30 7.14 3.57 4.18 7.72 5.74 3.85 5.58 6.90 4.23 7.48 5.74 4.42 10.49 6.83 4.28 8.79 5.66 9.65 9.79 7.16 6.9516:40 6.50 4.58 6.28 7.71 7.05 5.91 4.45 7.27 6.34 5.87 7.05 4.72 4.22 5.65 6.39 4.90 9.25 10.23 9.36 5.82 7.0716:50 5.78 4.33 5.34 8.32 5.74 6.57 4.98 8.47 5.40 8.12 5.74 6.82 8.12 6.65 5.45 5.92 6.07 6.66 9.87 6.44 7.7017:00 6.94 5.19 4.02 6.01 4.56 3.71 5.98 6.99 4.07 4.25 4.56 4.53 4.57 7.23 4.12 4.27 7.01 6.22 5.78 7.12 7.4517:10 6.26 2.13 4.14 4.60 4.68 6.31 4.96 5.83 4.19 4.58 4.68 4.67 5.85 8.50 4.24 5.24 5.74 9.46 5.93 8.43 4.9017:20 5.61 3.03 2.06 4.62 4.85 5.97 5.30 8.45 2.12 3.77 4.85 5.97 5.59 7.70 2.16 8.34 5.13 6.98 5.85 8.00 7.3217:30 5.00 2.02 2.58 4.37 5.21 4.99 4.45 9.26 2.64 6.80 5.21 6.98 6.50 4.58 2.69 4.33 3.30 6.90 4.74 5.19 7.9217:40 4.13 2.43 4.57 3.43 5.46 4.13 3.36 6.66 4.63 3.17 5.46 5.94 5.66 4.83 4.68 6.15 5.58 4.46 4.82 5.06 9.0917:50 4.89 4.19 3.89 2.99 4.36 5.65 5.59 7.86 3.94 2.82 4.36 4.93 5.22 4.88 3.99 3.99 4.36 5.33 4.20 4.66 7.6718:00 5.14 2.32 4.04 4.06 4.64 3.85 6.30 4.68 4.10 4.43 4.64 4.54 6.21 6.95 4.15 6.70 4.20 3.57 7.14 7.42 6.7018:10 3.65 2.73 4.26 6.90 3.75 5.84 3.64 5.23 7.89 6.49 3.75 4.27 4.18 5.06 6.35 2.71 3.71 3.72 2.60 5.28 6.2418:20 5.14 3.79 4.39 6.30 5.99 3.82 7.50 5.85 6.79 6.40 5.99 3.68 4.14 4.90 4.16 2.45 4.64 3.68 5.01 5.01 4.05

18:30 5.58 2.40 3.57 6.08 3.63 4.43 6.77 5.15 4.19 4.57 3.63 3.56 4.79 4.58 3.68 4.52 8.31 3.57 4.66 5.77 3.5718:40 4.99 2.85 3.72 5.87 3.26 5.47 2.82 4.14 4.60 4.45 3.26 3.61 4.16 4.49 3.83 6.44 3.42 1.76 3.50 4.17 3.7218:50 3.78 2.21 4.38 4.46 4.56 5.15 2.64 3.74 4.49 4.34 4.56 2.85 5.41 4.41 4.48 6.42 3.75 4.60 3.96 4.66 4.3819:00 3.94 2.41 3.84 4.18 3.79 3.15 3.90 4.59 4.95 4.05 3.79 4.15 0.50 4.40 5.23 4.60 4.24 4.43 4.13 4.12 5.12Max. 12.03 5.59 14.07 9.75 8.76 10.04 12.14 10.56 7.89 10.08 8.76 9.99 10.59 9.13 14.17 12.66 10.51 11.86 11.66 9.47 11.42Prom. 5.35 2.66 4.97 4.77 4.11 5.48 4.88 6.42 4.61 4.64 4.11 4.62 4.59 5.36 5.16 4.94 2.86 4.82 4.95 5.05 6.07Mín. 0.00 0.02 0.00 0.04 0.86 0.00 0.00 2.08 0.00 0.69 0.86 0.00 0.00 1.91 0.00 0.17 0.00 0.00 1.03 0.42 2.13

PERFILES DE VELOCIDAD DEL VIENTO (m/s), ZONA POSTERIOR DE LA FACULTAD DE EDUCACION DE LA UNS,(16 DE ENERO - 11 DE FEBRERO - 2006DETERMINACION DE LOS PARAMETROS DE WEIBULL

D I A S22 23 24 25 26 27 28 29 30 Velocidad Promedio = 4.85m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s m/s Vi (m/s) Xi mi 0.00 0.00 0.00 0.41 0.06 0.00 0.57 1.02 0.00 2.89 0.66 0.00 1.000 0.000 182 0.0833.93 0.00 0.00 0.10 0.03 0.00 3.24 1.51 0.00 3.93 0.94 0.00 2.000 0.693 122 0.0563.23 0.86 3.31 1.23 0.07 0.00 2.85 2.36 0.00 3.31 1.09 0.00 3.000 1.099 233 0.1062.82 0.33 2.83 0.00 0.01 0.00 2.98 0.98 0.00 4.44 1.07 0.00 4.000 1.386 174 0.0794.04 0.94 4.16 0.00 0.16 0.00 3.65 0.86 0.00 4.89 1.76 0.00 5.000 1.609 499 0.2282.01 0.00 2.98 1.17 0.27 0.00 2.43 1.96 0.00 4.77 1.73 0.00 6.000 1.792 270 0.1233.33 0.61 3.21 0.00 0.38 0.29 3.49 2.65 0.00 5.46 1.92 0.00 7.000 1.946 234 0.1072.14 0.53 4.22 1.31 0.58 0.53 2.16 2.49 0.00 5.01 1.98 0.00 8.000 2.079 221 0.1012.99 0.00 2.72 2.22 0.68 0.93 3.06 2.08 0.43 4.96 2.14 0.00 9.000 2.197 114 0.0525.67 2.12 4.61 1.13 0.64 1.34 5.76 3.75 0.80 5.91 2.70 0.00 10.000 2.303 84 0.0385.04 1.59 4.25 2.22 0.66 1.42 4.83 2.57 0.89 7.33 2.94 0.00 11.000 2.398 40 0.0185.96 1.22 2.40 1.44 0.78 1.77 5.68 2.32 1.15 5.96 2.70 0.00 12.000 2.485 12 0.0056.96 0.94 4.56 2.78 1.49 0.78 6.92 3.38 2.64 6.96 3.13 0.78 13.000 2.565 3 0.0014.09 0.21 3.55 0.00 2.41 2.77 4.05 1.96 1.54 5.34 2.56 0.00 14.000 2.639 0 0.0006.42 1.39 2.35 2.61 1.80 1.51 5.88 2.53 2.03 6.42 3.03 0.86 15.000 2.708 2 0.0014.64 0.65 4.67 3.88 2.69 1.88 4.37 3.06 3.19 5.46 3.04 0.65 2,1906.45 1.02 3.12 2.93 3.90 3.08 4.46 3.87 1.91 6.45 3.26 0.004.63 3.42 4.93 5.10 3.31 4.38 4.03 3.42 4.23 7.18 3.79 1.225.71 0.53 5.35 4.11 5.42 4.51 3.61 2.16 4.41 5.71 3.57 0.00 n° Xi Yi7.55 0.10 3.58 5.28 5.71 4.85 6.50 4.40 4.04 7.55 3.79 0.10 1 0.000 -2.4454.03 0.37 5.10 6.89 5.91 5.47 3.78 3.54 5.35 6.89 3.73 0.37 2 0.693 -1.9015.20 2.40 5.34 5.60 6.59 3.74 6.40 3.10 2.90 6.59 3.98 0.23 3 1.099 -1.268

4.08 2.97 3.52 5.70 4.24 6.55 4.05 2.65 3.36 6.55 3.59 0.23 4 1.386 -0.9354.36 0.31 5.26 6.66 5.85 5.07 4.03 3.54 5.75 6.78 3.81 0.00 5 1.609 -0.2188.39 1.22 3.66 7.79 6.20 7.62 8.31 2.97 4.16 8.39 4.49 1.22 6 1.792 0.119

9.64 2.04 4.70 4.95 5.51 8.31 9.99 1.71 6.16 9.99 4.46 0.77 7 1.946 0.4235.60 0.00 3.62 5.97 5.97 9.33 4.46 2.45 7.00 9.33 4.40 0.00 8 2.079 0.7667.70 0.04 5.11 6.45 4.49 9.53 7.71 2.28 6.65 9.53 4.78 0.04 9 2.197 1.0098.88 1.67 4.95 6.22 5.74 8.63 8.31 1.39 7.18 8.88 4.73 0.10 10 2.303 1.2945.33 0.90 5.59 7.77 6.60 7.35 5.25 5.30 3.47 10.60 5.22 0.30 11 2.398 1.5818.66 2.04 5.79 6.74 6.14 11.40 8.51 2.85 5.03 11.40 5.66 0.86 12 2.485 1.8059.48 0.00 5.12 7.72 5.71 5.95 9.77 6.68 7.37 10.22 5.92 0.00 13 2.565 1.946

Vmax VProm Vmin

P ( Vi ) mi/n

4.98 4.24 6.20 9.16 6.68 9.04 4.85 4.32 4.43 10.83 4.92 0.90 14 2.639 1.9467.20 3.30 4.97 5.84 4.64 7.66 6.90 1.67 6.83 12.03 5.77 0.907.24 2.00 3.96 8.38 4.44 7.37 6.50 4.85 4.63 9.53 5.89 2.00 Conocidos a y b entonces tenemos que los parametrso de weibull son :4.82 4.85 5.29 9.12 7.09 10.34 4.45 3.42 5.89 10.34 5.58 1.18 k = 2.0869.47 4.77 5.93 8.57 7.70 8.68 7.93 5.46 8.10 9.82 6.53 1.475.74 3.71 4.71 6.73 8.55 9.08 4.81 4.64 6.46 10.45 6.76 3.54 Estos para una velocidad promedio de :6.70 4.40 7.24 8.71 8.92 9.16 6.48 4.03 5.17 11.20 6.83 2.656.50 7.66 4.24 9.88 7.29 11.00 6.28 5.66 6.59 14.17 7.86 2.67 LUEGO :5.67 9.25 6.78 8.69 8.11 10.30 5.35 4.03 6.05 11.19 6.82 3.44 V W ( V )4.06 6.07 8.48 4.44 8.72 10.06 4.01 4.44 7.84 10.06 6.66 3.61 0.00 0.00006.23 7.01 10.07 9.77 9.12 10.30 5.87 4.81 6.90 10.30 7.29 2.86 1.00 0.06325.20 5.74 9.13 7.49 8.86 11.29 4.97 3.95 6.53 11.42 6.93 3.55 2.00 0.12117.34 5.13 5.91 6.37 8.72 7.36 7.49 7.98 6.37 10.59 7.10 2.55 3.00 0.15778.30 10.51 10.07 6.35 9.94 7.52 8.04 4.44 9.69 10.51 7.43 2.97 4.00 0.16727.63 4.03 6.61 7.74 10.00 7.64 6.91 2.20 7.60 10.00 6.61 2.20 5.00 0.15267.71 4.20 6.16 9.14 10.34 7.63 7.72 6.44 6.92 11.66 7.17 2.00 6.00 0.12286.59 7.05 7.26 9.16 9.33 7.75 7.54 8.76 9.16 9.92 7.65 3.86 7.00 0.08836.88 6.48 7.31 10.73 8.92 6.72 5.91 5.74 3.89 11.24 6.63 3.57 8.00 0.05714.30 5.46 9.87 5.10 10.14 5.06 4.05 6.44 5.48 10.35 6.79 3.88 9.00 0.03345.64 3.91 9.17 8.39 9.94 5.32 5.66 7.33 9.37 10.08 7.04 3.91 10.00 0.01762.54 3.95 6.46 6.20 10.06 4.85 2.84 6.76 5.63 12.66 6.54 2.54 11.00 0.00856.90 6.07 8.51 8.19 8.92 4.56 6.58 5.46 10.06 12.14 6.95 4.27 12.00 0.00376.84 4.52 9.06 8.38 10.34 4.36 5.67 4.52 10.87 11.86 7.42 3.71 13.00 0.00153.51 4.64 5.85 5.21 9.33 4.74 2.83 4.64 9.29 10.51 6.58 2.83 14.00 0.00056.80 6.44 3.88 5.07 9.94 4.67 3.57 6.44 4.10 10.31 6.22 3.036.21 3.30 6.05 5.66 8.31 5.20 5.08 5.78 8.59 10.49 6.34 3.303.32 5.74 6.96 7.00 7.58 6.70 4.14 5.58 10.71 10.71 6.48 3.326.29 4.85 7.96 5.30 8.92 6.21 5.87 5.82 7.12 9.87 6.56 4.338.71 5.70 8.16 7.82 8.74 7.44 8.54 5.70 6.12 8.74 6.05 3.714.71 5.38 6.80 7.33 7.90 8.21 4.85 5.38 5.68 9.46 5.72 2.134.83 6.64 7.33 6.23 7.86 8.98 5.25 6.64 6.65 8.98 5.80 2.067.67 5.99 3.21 4.92 8.31 8.81 6.91 5.99 6.64 9.26 5.47 2.024.14 6.39 5.52 4.79 6.88 9.10 4.05 6.52 5.62 9.10 5.22 2.433.71 4.56 4.98 4.99 6.74 8.20 3.48 4.44 5.04 8.20 4.86 2.823.87 6.80 2.19 3.72 7.11 7.52 3.75 4.60 3.00 7.52 4.95 2.194.06 7.74 3.93 1.89 7.29 7.84 3.52 2.53 4.64 7.89 4.72 1.895.98 3.42 7.42 2.96 6.07 6.73 6.07 2.57 4.04 7.50 4.96 2.45

0.0 2.0 4.0 6.0 8.0 10.0 12.0 14.0 16.00

0.02

0.04

0.06

0.08

0.1

0.12

0.14

0.16

0.18 DISTRIBUCION DE WEIBULL

V (m)

W (V

)

2.58 4.24 1.08 3.54 5.99 4.13 2.83 3.38 6.06 8.31 4.36 1.084.86 8.31 4.48 0.69 4.56 4.55 4.46 2.85 3.24 8.31 4.08 0.693.65 3.75 2.12 3.74 4.34 4.43 4.31 3.18 5.34 6.42 4.14 2.123.58 4.64 3.94 3.11 5.36 4.90 4.68 2.69 4.45 5.36 4.03 0.50

9.64 10.51 10.07 10.73 10.34 11.40 9.99 8.76 10.87 14.17 7.86 4.335.51 3.47 5.20 5.24 5.86 5.76 5.23 3.97 4.91 8.50 4.85 1.570.00 0.00 0.00 0.00 0.01 0.00 0.57 0.86 0.00 2.89 0.66 0.00

Resumen mensual

14.17 m/s4.85 m/s0.00 m/s

Vmax

VProm

VminJIFF :

IR a la Distribucion de Weibull

DETERMINACION DE LOS PARAMETROS DE WEIBULL DISTRIBUCION DE WEIBULLSabiendo que un mes trae 720 horas en promedio y un año trae 8760 horas.

m/sYi a b V ( m/s ) Horas de viento al mes P (W/m2) Horas de viento al año P (W/m2)

0.083 -2.445 1.410 -2.445 0 0.00 0.0 0.0 0.00.139 -1.901 1.940 -3.245 1 45.47 0.6 553.2 0.60.245 -1.268 2.313 -3.810 2 87.21 5.2 1061.1 5.20.325 -0.935 4.990 -7.853 3 113.55 17.5 1381.5 17.50.553 -0.218 0.986 -1.804 4 120.38 41.4 1464.6 41.40.676 0.119 1.545 -2.649 5 109.86 80.8 1336.7 80.80.783 0.423 1.696 -2.877 6 88.44 139.6 1076.0 139.60.884 0.766 1.900 -3.186 7 63.58 221.7 773.6 221.70.936 1.009 1.929 -3.229 8 41.11 331.0 500.2 331.00.974 1.294 2.032 -3.385 9 24.02 471.3 292.2 471.30.992 1.581 2.137 -3.543 10 12.71 646.4 154.6 646.40.998 1.805 2.177 -3.603 11 6.10 860.4 74.2 860.40.999 1.946 2.144 -3.555 12 2.66 1117.1 32.4 1117.10.999 1.946 2.004 -3.342 13 1.06 1420.3 12.8 1420.31.000 Err:502 14 0.38 1773.9 4.6 1773.9

Xpromedio = 1.510 DATOS TOMADOS PARA LA PARTE POSTERIOR DE LA UNS. (Nvo chimbote)

Ypromedio = -0.316

n° de pares = 14

Entonces :a b

2.086 -3.466

F ( Vi ) (acumulativo)

0 2 4 6 8 10 12 14 160

2

4

6

8

10

12

0.0

200.0

400.0

600.0

800.0

1000.0

1200.0

1400.0

1600.0

1800.0

2000.0CARACTERIZACION DEL POTENCIAL EOLICO MENSUAL (h = 10m)

V (m)

T(h/

mes

)

P (K

w/m

2)

Conocidos a y b entonces tenemos que los parametrso de weibull son :c = 5.2685 m/s m/s

Vp = 4.85 m/s

0.0 2.0 4.0 6.0 8.0 10.0 12.0 14.0 16.00

0.02

0.04

0.06

0.08

0.1

0.12

0.14

0.16

0.18 DISTRIBUCION DE WEIBULL

V (m)

W (V

)

0 2 4 6 8 10 12 14 160

2

4

6

8

10

12

0.0

200.0

400.0

600.0

800.0

1000.0

1200.0

1400.0

1600.0

1800.0

2000.0CARACTERIZACION DEL POTENCIAL EOLICO MENSUAL (h = 10m)

V (m)

T(h/

mes

)

P (K

w/m

2)

0 2 4 6 8 10 12 14 160

2

4

6

8

10

12

0.0

200.0

400.0

600.0

800.0

1000.0

1200.0

1400.0

1600.0

1800.0

2000.0CARACTERIZACION DEL POTENCIAL EOLICO ANUAL (h=10m)

V (m)

T (h

/año

)

P (K

w/m

2)

JIFF

JIFF

< ATRAS

IR a la Caracterizacion del Potencial Eolico

IR al Dimensionamiento del Alabe

< ATRAS

DIMENSIONAMIENTO DE UNA TURBINA EOLICA DATOS DE ENTRADA

V = 4.20 [m/s]02 al 04 [m] RANGO DEL DIAMETRO :1.2929 [kg/m3] mayor/igual que : 2.0000.4 menor /igual que : 4.000

0.85

0.95 RANGO DE LA VELOCIDAD :Z = 3 mayor/igual que : 2.0

menor /igual que : 6.0( De la distribucion de weibull )

POTENCIA TOTAL = 0.504 KW (SI SE DESEA SE PUEDE APROXIMAR LAPOTENCIA)

DETERMINACION DEL DIAMETRO OPTIMOV (m) D(m)2.00 34.62.50 24.83.00 18.83.50 14.94.00 12.24.50 10.35.00 8.85.50 7.66.00 6.7

V = 4.2V D (m) D (m) D (m) D (m) D (m)

(m/s) 14.9 12.2 10.3 8.8 7.6Cp Cp Cp Cp Cp

3.50 0.127 0.192 0.273 0.375 0.4994.00 0.086 0.128 0.183 0.251 0.3344.50 0.060 0.090 0.128 0.176 0.2355.00 0.044 0.066 0.094 0.128 0.1715.50 0.033 0.049 0.070 0.097 0.1286.00 0.026 0.038 0.054 0.074 0.099

Seleccionamos las combinaciones de V y D , mas convenientes :

D =r=

Cpmax =helec=hmec=

helec=0.85 hmec=0.95 r=1.2929

P (W) V (m/s) D (m) Cp nt504.49 4.50 14.95 0.060 0.049504.49 5.00 12.23 0.066 0.053504.49 5.50 10.25 0.070 0.057504.49 6.00 8.75 0.074 0.060504.49 0.00 7.59 #DIV/0! #DIV/0!504.49 0.00 6.66 #DIV/0! #DIV/0!

ENTONCES EL DIAMETRO Y LA VELOCIDAD SELECCIONADA SERAN :

Entonces :Diametro de rotor : D = 8.80 mArea de Barrido : A = 60.82 m2Velocidad Nominal : V = 4.20 m/sPotencia total : P = 500.00 WCoeficiente de Potencia : Cp = 0.375

Velocidad de giro del rotor (N): Velocidad de Supervivencia =

entonces : N = 129.9 rpmw = 13.6 rad/s

TSR = 14.3

Si el TSR resulta ser > 10 , entonces tendremos que darle una relacion para el multiplicador de La cual nos arrojara un valor mas apropiado del TSR :(Si no fuera asi dejarlo en 1/1 )

N = 43.3 rpmw = 4.5 rad/s

TSR = 4.75 TSR12

Determinacion del Coeficiente de solidez 34

Para TSR = 4.75 50.00 (introducir valor) 6

7Superficie total de las palas : 0.0000 m2 8Superficie para cada pala : 0.0000 m2 9

101112

Del grafico se tiene (W) =

0 2 4 6 8 10 120

10

20

30

40

50

60

70

80

Coeficiente de solidez

TSR

W(%)

Resistencia Aerodinamica del rotor : Faerod. = 0

Resistencia Aerodinamica de la pala : Faerod. = 0.000

DIMENSIONAMIENTO DEL ALABE DE LA TURBINA EOLICA

Como tendremos un TSR = 4.75 Usando el grafico de los perfiles NACA 4412 =>Cy/Cx = 0.99

PARAMETROS DE DISEÑO DE ENTRADA :Conclusion Parametros de diseño Velocidad 4.20 m/sDiametro 8.80 m

Radio 4.40 mArea 60.82 m2

Cp 0.38N 43.30 rpmw 4.53 rad/s

TSR 4.75Z 3.00 palas

Cy 0.99a 6.64 grados

ELECCION DEL PERFIL AERODINAMICO DE LA SECCION DEL ÁLABE ( Perfil NACA 4412)

Geometria aerodinamica del álabe del aerogenerador :r f C b

4.400 4.7501 7.93 0.355 1.294.290 4.6313 8.12 0.363 1.484.274 4.6144 8.15 0.365 1.514.253 4.5917 8.19 0.366 1.554.180 4.5126 8.33 0.372 1.694.107 4.4334 8.47 0.379 1.833.960 4.2751 8.78 0.392 2.143.850 4.1563 9.02 0.402 2.383.667 3.9584 9.45 0.420 2.813.300 3.5626 10.45 0.462 3.812.933 3.1667 11.68 0.513 5.042.200 2.3750 15.22 0.652 8.581.956 2.1111 16.90 0.713 10.261.650 1.7813 19.54 0.802 12.901.257 1.3572 24.26 0.937 17.621.015 1.0962 28.25 1.021 21.610.764 0.8244 33.67 1.082 27.030.671 0.7246 36.05 1.085 29.410.540 0.5833 39.83 1.059 33.190.400 0.4318 44.43 0.966 37.790.169 0.1827 53.10 0.571 46.460.112 0.1204 55.43 0.407 48.790.095 0.1023 56.11 0.354 49.47

tambien obtendremos del Grafico un CL = Para un angulo de ataque :

l r

0.086 0.0931 56.45 0.326 49.810.044 0.0470 58.21 0.079 51.570.000 0.0000 0.00 0.000 -6.64

LINEALIZACION DE PALA : Escogemos r = 0.8

r f C b4.400 3.800 9.83 0.358 3.1894.290 3.705 10.07 0.366 3.4304.274 3.691 10.11 0.367 3.4654.253 3.673 10.15 0.369 3.5134.180 3.610 10.32 0.374 3.6824.107 3.547 10.50 0.380 3.8583.960 3.420 10.87 0.393 4.2263.850 3.325 11.16 0.403 4.5193.667 3.167 11.68 0.421 5.0443.300 2.850 12.89 0.460 6.2502.933 2.533 14.36 0.507 7.7212.200 1.900 18.51 0.630 11.8661.956 1.689 20.42 0.680 13.7801.650 1.425 23.37 0.749 16.7331.257 1.086 28.43 0.839 21.7921.015 0.877 32.50 0.880 25.8620.764 0.660 37.73 0.884 31.0910.671 0.580 39.93 0.866 33.2950.540 0.467 43.32 0.815 36.683

l r

0.000

0.100

0.200

0.300

0.400

0.500

0.600

0.700

0.800

0.900

1.000

1.100

1.200

1.300

1.400

1.500

1.600

1.700

1.800

1.900

2.000

2.100

2.200

2.300

2.400

2.500

2.600

2.700

2.800

2.900

3.000

3.100

3.200

3.300

3.400

3.500

3.600

3.700

3.800

3.900

4.000

4.100

4.200

4.300

4.400

4.500

0

0.2

0.4

0.6

0.8

1

1.2

Perfil Aerodinamico del Alabe

r(m)

C(m

)

0.400 0.345 47.30 0.712 40.6560.169 0.146 54.46 0.392 47.8180.112 0.096 56.33 0.275 49.6950.095 0.082 56.88 0.238 50.2440.086 0.075 57.16 0.219 50.5210.044 0.038 58.57 0.115 51.9250.000 0.000 0.00 0.000 -6.640

GRAFICO DE LOS TAMAÑOS DE CUERDA SEGÚN EL DISEÑO AERODINAMICO Y LINEALIZADO :

r C1 C24.400 0.355 0.3584.290 0.363 0.3664.274 0.365 0.3674.253 0.366 0.3694.180 0.372 0.3744.107 0.379 0.3803.960 0.392 0.3933.850 0.402 0.4033.667 0.420 0.4213.300 0.462 0.4602.933 0.513 0.5072.200 0.652 0.6301.956 0.713 0.6801.650 0.802 0.7491.257 0.937 0.8391.015 1.021 0.8800.764 1.082 0.884

0.000

0.200

0.400

0.600

0.800

1.000

1.200

1.400

1.600

1.800

2.000

2.200

2.400

2.600

2.800

3.000

3.200

3.400

3.600

3.800

4.000

4.200

4.400

0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1

Geometria Linealizada del Alabe

r (m)

C (m

)

0.000

0.300

0.600

0.900

1.200

1.500

1.800

2.100

2.400

2.700

3.000

3.300

3.600

3.900

4.200

4.500

0.000

0.100

0.200

0.300

0.400

0.500

0.600

0.700

0.800

0.900

1.000

1.100

1.200 Geometria Aerodinamica vs Linealizada

r (m)

C (m

)

0.671 1.085 0.8660.540 1.059 0.8150.400 0.966 0.7120.169 0.571 0.3920.112 0.407 0.2750.095 0.354 0.2380.086 0.326 0.2190.044 0.079 0.115

0.000 0.000 0.000

PERFILES AERODINAMICOS NACA 4412

Upper Surface Lower SurfaceX/C Y/C X/C Y/C

0 0 0 01.25 2.44 1.25 -1.432.5 3.39 2.5 -1.955 4.73 5 -2.49

7.5 5.76 7.5 -2.7410 6.59 10 -2.8615 7.89 15 -2.8820 8.8 20 -2.7425 9.41 25 -2.530 9.76 30 -2.2640 9.8 40 -1.850 9.19 50 -1.460 8.14 60 -170 6.69 70 -0.6580 4.89 80 -0.3990 2.71 90 -0.2295 1.47 95 -0.16

100 0.13 100 -0.13100 0 100 0

r = 4.40 r = 4.18C = 0.358 C = 0.374

X Y (-Y) X Y0.00 0.00 0.00 0.00 0.000.45 0.87 -0.51 0.47 0.910.89 1.21 -0.70 0.94 1.271.79 1.69 -0.89 1.87 1.772.68 2.06 -0.98 2.81 2.163.58 2.36 -1.02 3.74 2.475.36 2.82 -1.03 5.62 2.957.15 3.15 -0.98 7.49 3.308.94 3.36 -0.89 9.36 3.52

10.73 3.49 -0.81 11.23 3.65

0.000

0.300

0.600

0.900

1.200

1.500

1.800

2.100

2.400

2.700

3.000

3.300

3.600

3.900

4.200

4.500

0.000

0.100

0.200

0.300

0.400

0.500

0.600

0.700

0.800

0.900

1.000

1.100

1.200 Geometria Aerodinamica vs Linealizada

r (m)

C (m

)

14.30 3.50 -0.64 14.98 3.6717.88 3.29 -0.50 18.72 3.4421.45 2.91 -0.36 22.47 3.0525.03 2.39 -0.23 26.21 2.5128.60 1.75 -0.14 29.96 1.8332.18 0.97 -0.08 33.70 1.0133.96 0.53 -0.06 35.57 0.5535.75 0.05 -0.05 37.45 0.0535.75 0.00 0.00 37.45 0.00

r = 2.20 r = 1.96C = 0.630 C = 0.680

X Y (-Y) X Y0.00 0.00 0.00 0.00 0.000.79 1.54 -0.90 0.85 1.661.57 2.13 -1.23 1.70 2.313.15 2.98 -1.57 3.40 3.224.72 3.63 -1.73 5.10 3.926.30 4.15 -1.80 6.80 4.489.45 4.97 -1.81 10.20 5.37

12.59 5.54 -1.73 13.60 5.9915.74 5.93 -1.57 17.01 6.4018.89 6.15 -1.42 20.41 6.6425.19 6.17 -1.13 27.21 6.6731.49 5.79 -0.88 34.01 6.2537.78 5.13 -0.63 40.81 5.5444.08 4.21 -0.41 47.62 4.5550.38 3.08 -0.25 54.42 3.3356.67 1.71 -0.14 61.22 1.8459.82 0.93 -0.10 64.62 1.0062.97 0.08 -0.08 68.02 0.0962.97 0.00 0.00 68.02 0.00

r = 0.67 r = 0.54C = 0.866 C = 0.815

X Y (-Y) X Y0.00 0.00 0.00 0.00 0.001.08 2.11 -1.24 1.02 1.992.17 2.94 -1.69 2.04 2.764.33 4.10 -2.16 4.08 3.866.50 4.99 -2.37 6.11 4.698.66 5.71 -2.48 8.15 5.37

13.00 6.84 -2.50 12.23 6.4317.33 7.63 -2.37 16.30 7.1721.66 8.15 -2.17 20.38 7.6725.99 8.46 -1.96 24.45 7.9634.66 8.49 -1.56 32.60 7.9943.32 7.96 -1.21 40.75 7.4951.99 7.05 -0.87 48.90 6.63

60.65 5.80 -0.56 57.05 5.4569.32 4.24 -0.34 65.21 3.9977.98 2.35 -0.19 73.36 2.2182.32 1.27 -0.14 77.43 1.2086.65 0.11 -0.11 81.51 0.1186.65 0.00 0.00 81.51 0.00

JIFF

< ATRAS

IR AL CUADRO DE RESUMEN FINAL

DIMENSIONAMIENTO DE UNA TURBINA EOLICAELECCION DE LA POTENCIA A GENERAR

RANGO DE VELOCIDADES (m/s)D (m) A (m2) 2.0 3.0 4.0 5.0 6.0 P (kw)

2.0 3.1415 0.01625 0.054832 0.12997 0.253853 0.43866 0.178712.5 4.908594 0.02539 0.085675 0.20308 0.396645 0.6854 0.27924

3.0 7.068375 0.03655 0.123372 0.29244 0.571169 0.98698 0.4021

3.5 9.620844 0.04976 0.167924 0.39804 0.777424 1.34339 0.547314.0 12.566 0.06499 0.219329 0.51989 1.015411 1.75463 0.714854.5 15.90384 0.08225 0.277588 0.65799 1.28513 2.2207 0.90473

Potencia Seleccionada = 0.50449

(SI SE DESEA SE PUEDE APROXIMAR LAPOTENCIA) 0.5 KW

D (m)6.7Cp

0.6470.4340.3050.2220.1670.128

Opcionabcdefg

D(m) P(W) V (m/s) Cp 8.80 500.00 3.50 0.375

60 m/s

3 / 1

W80502515107532

1.51.21

0 2 4 6 8 10 120

10

20

30

40

50

60

70

80

Coeficiente de solidez

TSR

W(%)

kg

kg

DIMENSIONAMIENTO DEL ALABE DE LA TURBINA EOLICA

Usando el grafico de los perfiles NACA 4412 =>Cy/Cx = 85.9 optimo6.64

POTENCIA AL EJE

500.00 W

ELECCION DEL PERFIL AERODINAMICO DE LA SECCION DEL ÁLABE ( Perfil NACA 4412)

0.9904480.9899670.9898960.989799

0.989450.989083

0.988290.9876370.9864240.9834050.9792810.9649150.956828

0.942410.91172

0.8809010.83229

0.8085150.7679620.7141140.6004530.5674970.557632

Para un angulo de ataque : =a

COS f

0.5526270.526883

R

0.9853220.9845960.9844880.9843430.9838170.9832640.9820720.9810940.9792810.9748010.9687550.9482940.9371620.9179440.8793930.8433840.7909070.7667890.727512

COS f

0.000

0.100

0.200

0.300

0.400

0.500

0.600

0.700

0.800

0.900

1.000

1.100

1.200

1.300

1.400

1.500

1.600

1.700

1.800

1.900

2.000

2.100

2.200

2.300

2.400

2.500

2.600

2.700

2.800

2.900

3.000

3.100

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3.400

3.500

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4.000

4.100

4.200

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4.500

0

0.2

0.4

0.6

0.8

1

1.2

Perfil Aerodinamico del Alabe

r(m)

C(m

)

0.6782280.5813210.554365

0.546360.5423080.521553

GRAFICO DE LOS TAMAÑOS DE CUERDA SEGÚN EL DISEÑO AERODINAMICO Y LINEALIZADO :

0.000

0.200

0.400

0.600

0.800

1.000

1.200

1.400

1.600

1.800

2.000

2.200

2.400

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2.800

3.000

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4.400

0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1

Geometria Linealizada del Alabe

r (m)

C (m

)

0.000

0.300

0.600

0.900

1.200

1.500

1.800

2.100

2.400

2.700

3.000

3.300

3.600

3.900

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4.500

0.000

0.100

0.200

0.300

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0.600

0.700

0.800

0.900

1.000

1.100

1.200 Geometria Aerodinamica vs Linealizada

r (m)

C (m

)

PERFILES AERODINAMICOS NACA 4412

CUERDA RADIOC(m) r (m)0.358 4.400.374 4.180.403 3.850.421 3.670.460 3.300.507 2.930.630 2.200.680 1.960.749 1.650.839 1.260.880 1.020.884 0.760.866 0.670.815 0.540.712 0.400.392 0.170.238 0.090.115 0.040.000 0.00

r = 3.85 r = 3.67 r = 3.30C = 0.403 C = 0.421 C = 0.460

(-Y) X Y (-Y) X Y (-Y) X Y0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00-0.54 0.50 0.98 -0.58 0.53 1.03 -0.60 0.58 1.12-0.73 1.01 1.37 -0.79 1.05 1.43 -0.82 1.15 1.56-0.93 2.01 1.91 -1.00 2.10 1.99 -1.05 2.30 2.18-1.03 3.02 2.32 -1.10 3.15 2.42 -1.15 3.45 2.65-1.07 4.03 2.66 -1.15 4.21 2.77 -1.20 4.60 3.03-1.08 6.04 3.18 -1.16 6.31 3.32 -1.21 6.90 3.63-1.03 8.06 3.55 -1.10 8.41 3.70 -1.15 9.21 4.05-0.94 10.07 3.79 -1.01 10.51 3.96 -1.05 11.51 4.33-0.85 12.09 3.93 -0.91 12.62 4.10 -0.95 13.81 4.49

0.000

0.300

0.600

0.900

1.200

1.500

1.800

2.100

2.400

2.700

3.000

3.300

3.600

3.900

4.200

4.500

0.000

0.100

0.200

0.300

0.400

0.500

0.600

0.700

0.800

0.900

1.000

1.100

1.200 Geometria Aerodinamica vs Linealizada

r (m)

C (m

)

0.00 10.00 20.00 30.00 40.00 50.00 60.00 70.00 80.00

-4.00

-2.00

0.00

2.00

4.00

6.00

8.00

Peril Aerodinamico NACA 4412 para r = 0.46 y C =0.22

-0.67 16.12 3.95 -0.73 16.82 4.12 -0.76 18.41 4.51-0.52 20.15 3.70 -0.56 21.03 3.86 -0.59 23.02 4.23-0.37 24.18 3.28 -0.40 25.23 3.42 -0.42 27.62 3.75-0.24 28.21 2.70 -0.26 29.44 2.81 -0.27 32.22 3.08-0.15 32.23 1.97 -0.16 33.64 2.06 -0.16 36.83 2.25-0.08 36.26 1.09 -0.09 37.85 1.14 -0.09 41.43 1.25-0.06 38.28 0.59 -0.06 39.95 0.62 -0.07 43.73 0.68-0.05 40.29 0.05 -0.05 42.05 0.05 -0.05 46.03 0.060.00 40.29 0.00 0.00 42.05 0.00 0.00 46.03 0.00

r = 1.65 r = 1.26 r = 1.02C = 0.749 C = 0.839 C = 0.880

(-Y) X Y (-Y) X Y (-Y) X Y0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00-0.97 0.94 1.83 -1.07 1.05 2.05 -1.20 1.10 2.15-1.33 1.87 2.54 -1.46 2.10 2.85 -1.64 2.20 2.98-1.69 3.75 3.55 -1.87 4.20 3.97 -2.09 4.40 4.16-1.86 5.62 4.32 -2.05 6.29 4.83 -2.30 6.60 5.07-1.95 7.49 4.94 -2.14 8.39 5.53 -2.40 8.80 5.80-1.96 11.24 5.91 -2.16 12.59 6.62 -2.42 13.20 6.95-1.86 14.99 6.60 -2.05 16.79 7.39 -2.30 17.61 7.75-1.70 18.74 7.05 -1.87 20.98 7.90 -2.10 22.01 8.28-1.54 22.48 7.31 -1.69 25.18 8.19 -1.90 26.41 8.59-1.22 29.98 7.34 -1.35 33.57 8.23 -1.51 35.21 8.63-0.95 37.47 6.89 -1.05 41.97 7.71 -1.18 44.02 8.09-0.68 44.97 6.10 -0.75 50.36 6.83 -0.84 52.82 7.17-0.44 52.46 5.01 -0.49 58.75 5.62 -0.55 61.62 5.89-0.27 59.96 3.66 -0.29 67.15 4.10 -0.33 70.43 4.30-0.15 67.45 2.03 -0.16 75.54 2.27 -0.18 79.23 2.39-0.11 71.20 1.10 -0.12 79.74 1.23 -0.13 83.63 1.29-0.09 74.95 0.10 -0.10 83.93 0.11 -0.11 88.03 0.110.00 74.95 0.00 0.00 83.93 0.00 0.00 88.03 0.00

r = 0.40 r = 0.17 r = 0.09C = 0.712 C = 0.392 C = 0.238

(-Y) X Y (-Y) X Y (-Y) X Y0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00-1.17 0.89 0.65 -1.02 0.49 0.96 -0.56 0.30 0.58-1.59 1.78 0.91 -1.39 0.98 1.33 -0.76 0.59 0.81-2.03 3.56 1.27 -1.77 1.96 1.86 -0.98 1.19 1.13-2.23 5.34 1.54 -1.95 2.94 2.26 -1.07 1.78 1.37-2.33 7.12 1.77 -2.04 3.92 2.58 -1.12 2.38 1.57-2.35 10.69 2.11 -2.05 5.88 3.09 -1.13 3.57 1.88-2.23 14.25 2.36 -1.95 7.84 3.45 -1.07 4.76 2.09-2.04 17.81 2.52 -1.78 9.81 3.69 -0.98 5.95 2.24-1.84 21.37 2.62 -1.61 11.77 3.83 -0.89 7.14 2.32-1.47 28.50 2.63 -1.28 15.69 3.84 -0.71 9.51 2.33-1.14 35.62 2.46 -1.00 19.61 3.60 -0.55 11.89 2.19-0.82 42.75 2.18 -0.71 23.53 3.19 -0.39 14.27 1.94

-0.53 49.87 1.79 -0.46 27.46 2.62 -0.25 16.65 1.59-0.32 57.00 1.31 -0.28 31.38 1.92 -0.15 19.03 1.16-0.18 64.12 0.73 -0.16 35.30 1.06 -0.09 21.41 0.64-0.13 67.69 0.39 -0.11 37.26 0.58 -0.06 22.60 0.35-0.11 71.25 0.03 -0.09 39.22 0.05 -0.05 23.79 0.030.00 71.25 0.00 0.00 39.22 0.00 0.00 23.79 0.00

JIFF

< ATRAS

IR AL CUADRO DE RESUMEN FINAL

DIMENSIONAMIENTO DE UNA TURBINA EOLICA

r = 2.93C = 0.507

(-Y) X Y (-Y)0.00 0.00 0.00 0.00-0.66 0.63 1.24 -0.73-0.90 1.27 1.72 -0.99-1.15 2.54 2.40 -1.26-1.26 3.81 2.92 -1.39-1.32 5.07 3.34 -1.45-1.33 7.61 4.00 -1.46-1.26 10.15 4.46 -1.39-1.15 12.68 4.77 -1.27-1.04 15.22 4.95 -1.15

0.00 10.00 20.00 30.00 40.00 50.00 60.00 70.00 80.00

-4.00

-2.00

0.00

2.00

4.00

6.00

8.00

Peril Aerodinamico NACA 4412 para r = 0.46 y C =0.22

-0.83 20.29 4.97 -0.91-0.64 25.37 4.66 -0.71-0.46 30.44 4.13 -0.51-0.30 35.52 3.39 -0.33-0.18 40.59 2.48 -0.20-0.10 45.66 1.37 -0.11-0.07 48.20 0.75 -0.08-0.06 50.74 0.07 -0.070.00 50.74 0.00 0.00

r = 0.76C = 0.884

(-Y) X Y (-Y)0.00 0.00 0.00 0.00-1.26 1.10 2.16 -1.26-1.72 2.21 3.00 -1.72-2.19 4.42 4.18 -2.20-2.41 6.63 5.09 -2.42-2.52 8.84 5.82 -2.53-2.54 13.26 6.97 -2.55-2.41 17.68 7.78 -2.42-2.20 22.10 8.32 -2.21-1.99 26.52 8.63 -2.00-1.58 35.36 8.66 -1.59-1.23 44.19 8.12 -1.24-0.88 53.03 7.19 -0.88-0.57 61.87 5.91 -0.57-0.34 70.71 4.32 -0.34-0.19 79.55 2.40 -0.19-0.14 83.97 1.30 -0.14-0.11 88.39 0.11 -0.110.00 88.39 0.00 0.00

r = 0.04C = 0.115

(-Y) X Y (-Y)0.00 0.00 0.00 0.00-0.34 0.14 0.28 -0.16-0.46 0.29 0.39 -0.22-0.59 0.58 0.55 -0.29-0.65 0.87 0.66 -0.32-0.68 1.15 0.76 -0.33-0.69 1.73 0.91 -0.33-0.65 2.31 1.02 -0.32-0.59 2.88 1.09 -0.29-0.54 3.46 1.13 -0.26-0.43 4.62 1.13 -0.21-0.33 5.77 1.06 -0.16-0.24 6.92 0.94 -0.12

-0.15 8.08 0.77 -0.07-0.09 9.23 0.56 -0.04-0.05 10.38 0.31 -0.03-0.04 10.96 0.17 -0.02-0.03 11.54 0.01 -0.010.00 11.54 0.00 0.00

CUADRO RESUMEN DE TODOS LOS CALCULOS DE DISEÑO

DATOS DE ENTRADA PARA LA DISTRIBUCION DE WEIBULL :

Valor intermedio para los Parametro de Forma: K = 2.09valores de diametro(m) Parametro de Escala: c = 5.27

Entre ### y ### PARA EL DIMENSIONAMIENTO DEL LUGAR :

Velocidad promedio Velocidad del Lugar = 4.2 m/s

Vm = 4.20 m/s Potencia total a Generar = 500.00 w

Diametro del Rotor = 8.80 m

Area de Barrido = 60.82 m2

Velocidad de giro del Rotor = 43.30 rpm

Velocidad angular = 4.53 rad/s

4.75 Cp = 0.375

0.99 Z = 3

=l TSR =

CL =

JIFF VER EL PERFIL LINEALIZADO FINAL

< ATRAS

CUADRO RESUMEN DE TODOS LOS CALCULOS DE DISEÑO

PARA LA DISTRIBUCION DE WEIBULL :

PARA EL DIMENSIONAMIENTO DEL LUGAR :

=a 6.64

0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 50

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1

r (m)

C (m

)

0.00 10.00 20.00 30.00 40.00 50.00 60.00 70.00 80.00

-4.00

-2.00

0.00

2.00

4.00

6.00

8.00

JIFF

0.00 10.00 20.00 30.00 40.00 50.00 60.00 70.00 80.00

-4.00

-2.00

0.00

2.00

4.00

6.00

8.00

PERFIL DE PALA LINEALIZADA4.4 0.35751211

4.29 0.365807114.27428571 0.367021824.25333333 0.3686533

4.18 0.374472494.10666667 0.38046662

3.96 0.393009383.85 0.402932843.66666667 0.420541643.3 0.460320422.93333333 0.507360592.2 0.629705461.95555556 0.680241371.65 0.749487121.25714286 0.839322721.01538462 0.880315570.76363636 0.883889320.67118644 0.8664890.54035088 0.81507011

0.4 0.71249050.16923077 0.392221690.11150097 0.275060930.09471624 0.237852040.08627451 0.218588540.04356436 0.11538158

0 0

PERFIL NACA 4412 PARA UN r = 0.22 y C =

0.00 0.00 0.000.85 1.66 -0.971.70 2.31 -1.333.40 3.22 -1.695.10 3.92 -1.866.80 4.48 -1.95

10.20 5.37 -1.9613.60 5.99 -1.8617.01 6.40 -1.7020.41 6.64 -1.5427.21 6.67 -1.2234.01 6.25 -0.9540.81 5.54 -0.6847.62 4.55 -0.4454.42 3.33 -0.2761.22 1.84 -0.1564.62 1.00 -0.1168.02 0.09 -0.0968.02 0.00 0.00

0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 50

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1

r (m)

C (m

)

0.00 10.00 20.00 30.00 40.00 50.00 60.00 70.00 80.00

-4.00

-2.00

0.00

2.00

4.00

6.00

8.00

0.00 10.00 20.00 30.00 40.00 50.00 60.00 70.00 80.00

-4.00

-2.00

0.00

2.00

4.00

6.00

8.00

JIFF

ANEXOS

FIN !! (volver a la portada)

ANEXOS

NACA 4412

Valores estimados de eficiencia

Datos de Aeroturbinas tipo helice

Numero de palas en funcion del TSR

JIFFFIN !!

PERFIL DE PALA LINEALIZADA

PERFIL NACA 4412 PARA UN r = 0.22 y C =

0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 50

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1

r (m)

C (m

)

0.00 10.00 20.00 30.00 40.00 50.00 60.00 70.00 80.00

-4.00

-2.00

0.00

2.00

4.00

6.00

8.00

0.00 10.00 20.00 30.00 40.00 50.00 60.00 70.00 80.00

-4.00

-2.00

0.00

2.00

4.00

6.00

8.00

JIFF

ANEXOS

Coeficiente de solidez vs TSR

Valores estimados de eficiencia

Datos de Aeroturbinas tipo helice

Numero de palas en funcion del TSR

JIFFFIN !!