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Ejercicio2

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Ejercicio de Rigidez Directa

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  • 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