of 26
MATRICES RIGIDEZ, TRANSFORMACION
ELEMENTO PORTICO 1
L1 = 14.142
0.7071 0.7071 0.0000-0.7071 0.7071 0.0000
T1 = 0.0000 0.0000 1.00000.0000 0.0000 0.00000.0000 0.0000 0.00000.0000 0.0000 0.0000
54094.0 0.0 0.00.0 357020.0 2524500.0
KL1 = 0.0 2524500.0 23801000.0-54094.0 0.0 0.00.0 -357020.0 -2524500.00.0 2524500.0 11901000.0
10 11 12205560.0 -151460.0 -1785100.0-151460.0 205560.0 1785100.0
K1 = -1785100.0 1785100.0 23801000.0-205560.0 151460.0 1785100.0151460.0 -205560.0 -1785100.0
-1785100.0 1785100.0 11901000.0
ELEMENTO PORTICO 2
L2 = 14.142
0 1 0-1 0 0
T2 = 0 0 10 0 00 0 00 0 0
72125.0 0.0 0.00.0 357020.0 2524500.0
KL2 = 0.0 2524500.0 23801000.0-72125.0 0.0 0.00.0 -357020.0 -2524500.00.0 2524500.0 11901000.0
8 9 6357020.0 0.0 -2524500.0
0.0 72125.0 0.0
K2 = -2524500.0 0.0 23801000.0252450.0 -51000.0 -1785100.0252450.0 51000.0 -1785100.0
-2524500.0 0.0 11901000.0
ELEMENTO PORTICO 3
L3 = 14.142
0.70711 0.70711 0-0.70711 0.70711 0
T3 = 0 0 10 0 00 0 00 0 0
54094.0 0.0 0.00.0 357020.0 2524500.0
KL3 = 0.0 2524500.0 23801000.0-54094.0 0.0 0.00.0 -357020.0 -2524500.00.0 2524500.0 11901000.0
1 2 3205560.0 -151460.0 -1785100.0-151460.0 205560.0 1785100.0
K3 = -1785100.0 1785100.0 23801000.0252450.0 -252450.0 -2524500.038250.0 38250.0 0.0
-1785100.0 1785100.0 11901000.0
ELEMENTO PORTICO 4
L4 = 14.142
0.7071 -0.7071 0.00000.7071 0.7071 0.0000
T4 = 0.0000 0.0000 1.00000.0000 0.0000 0.0000
0.0000 0.0000 0.00000.0000 0.0000 0.0000
72125.0 0.0 0.00.0 357020.0 2524500.0
KL4 = 0.0 2524500.0 23801000.0-72125.0 0.0 0.00.0 -357020.0 -2524500.00.0 2524500.0 11901000.0
1 2 3214570.0 142450.0 1785100.0142450.0 214570.0 1785100.0
K4 = 1785100.0 1785100.0 23801000.0-214570.0 -142450.0 -1785100.0-142450.0 -214570.0 -1785100.01785100.0 1785100.0 11901000.0
ELEMENTOBIARTICULADO 5
L5 = 20
T5 = -0.70711 0.70711 00 0 -0.70711
KL5 = 40000 -40000-40000 40000
8 9 420000 -20000 -20000
K5 = -20000 20000 20000-20000 20000 20000-20000 20000 20000
Matriz de Rigidez de toda la Estructura
1 2 3 4 5840250.0 -18031.0 0.0 252450.0 -1785100.0-18031.0 840250.0 0.0 -252450.0 1785100.0
Kuu = 0.0 0.0 95205000.0 -2524500.0 11901000.0252450.0 -252450.0 -2524500.0 377020.0 -2524500.0-1785100.0 1785100.0 11901000.0 -2524500.0 23801000.0-1785100.0 -1785100.0 11901000.0 0.0 0.0
7 8 9 10 1138250.0 252450.0 -51000.0 -205560.0 151460.038250.0 252450.0 51000.0 151460.0 -205560.0
Kur = 0.0 -2524500.0 0.0 -1785100.0 1785100.020000.0 -20000.0 20000.0 0.0 0.00.0 0.0 0.0 0.0 0.00.0 -2524500.0 0.0 0.0 0.0
1 2 3 4 538250.0 38250.0 0.0 20000.0 0.0
252450.0 252450.0 -2524500.0 -20000.0 0.0-51000.0 51000.0 0.0 20000.0 0.0
-205560.0 151460.0 -1785100.0 0.0 0.0Kru = 151460.0 -205560.0 1785100.0 0.0 0.0
1785100.0 -1785100.0 11901000.0 0.0 0.0-214570.0 -142450.0 -1785100.0 0.0 0.0-142450.0 -214570.0 -1785100.0 0.0 0.01785100.0 1785100.0 11901000.0 0.0 0.0
7 8 9 10 1174094.0 -20000.0 20000.0 0.0 0.0-20000.0 377020.0 -20000.0 0.0 0.020000.0 -20000.0 92125.0 0.0 0.0
0.0 0.0 0.0 205560.0 -151460.0Krr = 0.0 0.0 0.0 -151460.0 205560.0
0.0 0.0 0.0 -1785100.0 1785100.00.0 0.0 0.0 0.0 0.00.0 0.0 0.0 0.0 0.00.0 0.0 0.0 0.0 0.0
VECTORES DE CARGA " FUERZAS "
Fuerzas Nodales
12 10 22 30 40 50 60 7
Fn = 0 80 90 100 110 120 130 140 15
FUERZAS DE EMPOTRAMIENTO LOCAL
-14.142014.1420
FEL1 = 33.3330-14.142014.1420-33.3330
00
FEL2 = 0000
00
FEL3 = 0000
00
FEL4 = 0000
FUERZAS DE EMPOTRAMIENTO GLOBAL
-20 100 11
FEG1 = 33.333 12-20 10 2
-33.333 3
0 80 9
FEG2 = 0 60 10 20 3
0 10 2
FEG3 = 0 30 40 70 5
0 10 2
FEG4 = 0 30 130 140 15
Vector de Fuerzas de Empotramiento Ensamblado
-20 10 2
-33.333 30 40 50 60 7
Fe = 0 80 9
-20 100 11
33.333 120 130 140 15
FUERZAS DE TODA LA ESTRUCTURA
Fuerzas Libres
32 10 2
Fu = 35.333 30 40 50 6
Fuerzas Restringidas
0 70 80 9
20 10Fre = 0 11
-33.333 120 130 140 15
Desplazamientos Restringidos
0 70 80 90 10
Dr = 0 110 120 130 140 15
RESULTADOS
Desplazamientos Libres
0.000069686 1-5.2398E-006 2
Du = -2.0910E-006 3-6.7439E-005 4-4.8814E-007 55.8789E-006 6
Reacciones =
1.1163 78.0555 8-5.17 9
-31.385 10
Fr = 7.8992 11142.2 12-10.474 13-5.0696 1490.158 15
Desplazamientos de toda la Estructura
0.000069686 1-5.2398E-006 2-2.0910E-006 3-6.7439E-005 4-4.8814E-007 55.8789E-006 6
0 7
D = 0 80 90 100 110 120 130 140 15
Fuerzas Internas
-16.60727.778
Fi 1 = 142.2-11.6770.5058950.648
-3.8212-6.7067
Fi 2 = -7.1054E-0153.82126.7067-94.847
2.465-1.3488
Fi 3 = -19.075-2.4651.3488
-1.0303E-013
3.821210.991
Fi 4 = 65.274-3.8212-10.99190.158
Fi 5 = 2.6976-2.6976
MATRICES RIGIDEZ, TRANSFORMACION
0.0000 0.0000 0.00000.0000 0.0000 0.00000.0000 0.0000 0.00000.7071 0.7071 0.0000-0.7071 0.7071 0.00000.0000 0.0000 1.0000
-54094.0 0.0 0.00.0 -357020.0 2524500.00.0 -2524500.0 11901000.0
54094.0 0.0 0.00.0 357020.0 -2524500.00.0 -2524500.0 23801000.0
1 2 3-205560.0 151460.0 -1785100.0 10151460.0 -205560.0 1785100.0 11
1785100.0 -1785100.0 11901000.0 12205560.0 -151460.0 1785100.0 1-151460.0 205560.0 -1785100.0 21785100.0 -1785100.0 23801000.0 3
0 0 00 0 00 0 0
0.70711 -0.70711 00.70711 0.70711 0
0 0 1
-72125.0 0.0 0.00.0 -357020.0 2524500.0
0.0 -2524500.0 11901000.072125.0 0.0 0.0
0.0 357020.0 -2524500.00.0 -2524500.0 23801000.0
1 2 3252450.0 252450.0 -2524500.0 8-51000.0 51000.0 0.0 9
-1785100.0 -1785100.0 11901000.0 6214570.0 142450.0 -1785100.0 1142450.0 214570.0 -1785100.0 2
-1785100.0 -1785100.0 23801000.0 3
0 0 00 0 00 0 00 -1 01 0 00 0 1
-54094.0 0.0 0.00.0 -357020.0 2524500.00.0 -2524500.0 11901000.0
54094.0 0.0 0.00.0 357020.0 -2524500.00.0 -2524500.0 23801000.0
4 7 5252450.0 38250.0 -1785100.0 1-252450.0 38250.0 1785100.0 2
-2524500.0 0.0 11901000.0 3357020.0 0.0 -2524500.0 4
0.0 54094.0 0.0 7-2524500.0 0.0 23801000.0 5
0.0000 0.0000 0.00000.0000 0.0000 0.00000.0000 0.0000 0.00000.7071 -0.7071 0.0000
0.7071 0.7071 0.00000.0000 0.0000 1.0000
-72125.0 0.0 0.00.0 -357020.0 2524500.00.0 -2524500.0 11901000.0
72125.0 0.0 0.00.0 357020.0 -2524500.00.0 -2524500.0 23801000.0
13 14 15-214570.0 -142450.0 1785100.0 1-142450.0 -214570.0 1785100.0 2
-1785100.0 -1785100.0 11901000.0 3214570.0 142450.0 -1785100.0 13142450.0 214570.0 -1785100.0 14
-1785100.0 -1785100.0 23801000.0 15
0-0.70711
7-20000 820000 920000 420000 7
6-1785100.0 1-1785100.0 211901000.0 3
0.0 40.0 5
23801000.0 6
12 13 14 151785100.0 -214570.0 -142450.0 1785100.0 1-1785100.0 -142450.0 -214570.0 1785100.0 211901000.0 -1785100.0 -1785100.0 11901000.0 3
0.0 0.0 0.0 0.0 40.0 0.0 0.0 0.0 50.0 0.0 0.0 0.0 6
60.0 7
-2524500.0 80.0 90.0 100.0 110.0 120.0 130.0 140.0 15
12 13 14 150.0 0.0 0.0 0.0 70.0 0.0 0.0 0.0 80.0 0.0 0.0 0.0 9
-1785100.0 0.0 0.0 0.0 101785100.0 0.0 0.0 0.0 11
23801000.0 0.0 0.0 0.0 120.0 214570.0 142450.0 -1785100.0 130.0 142450.0 214570.0 -1785100.0 140.0 -1785100.0 -1785100.0 23801000.0 15
VECTORES DE CARGA " FUERZAS "
FUERZAS DE EMPOTRAMIENTO GLOBAL
Vector de Fuerzas de Empotramiento Ensamblado
F = Fn-Fe
32 10 2
35.333 30 40 50 60 7
F = 0 80 9
20 100 11
-33.333 120 130 140 15
RESULTADOS
Desplazamientos de toda la Estructura
Ejercicio