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Exam (elaborations)

Structural Dynamics Theory and Computation Sixth Edition Mario Paz - Complete Solution Manual

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This comprehensive solution manual accompanies "Structural Dynamics: Theory and Computation" Sixth Edition by Mario Paz. It provides detailed step-by-step solutions to all problems across 21 chapters covering fundamental concepts of structural dynamics including free and forced vibration of single-degree-of-freedom systems, multi-degree-of-freedom systems, distributed parameter systems, damping theory, response spectra, earthquake analysis, matrix methods, and computational approaches. Perfect for civil engineering, mechanical engineering, and aerospace engineering students studying structural dynamics, vibration analysis, and earthquake engineering.

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Institution
Structural Dynamics Theory And Computation
Course
Structural Dynamics Theory and Computation

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Solution Manual for Structural Dynamics Theory and Comput
o o o o o o o



ation Sixth Edition by Paz
o o o o




1

,1.1


Ifotheoweightowoisodisplacedobyoamount,oy,otheobeamoandotheospringsowilloexertoaototaloforceoo
notheomassoof
3𝐸𝐼o
𝑃o=o# +o2𝑘,o𝑢
𝐿(

Theobeamoandospringsoactoinoparallel.oTheoequivalentostiffnessois:
𝑃o 3𝐸𝐼o
𝑘o o =o =o # +o2𝑘,
.
𝑢 𝐿(

Naturalofrequency:

𝑘 𝑔 3𝐸𝐼
𝜔o=o0
o o
=o0 # +o2𝑘,
𝑚 𝑊 𝐿(

Naturaloperiod:

2𝜋o 𝑊o 𝐿
𝑇 o =o =o 2𝜋𝐿0 # ,
𝜔 𝑔 3𝐸𝐼o+o2𝑘𝐿 (




1.2


Stiffness:

3𝐸𝐼 3o×o109
𝑘.o=o#o (o +o2𝑘,o +o2o×o1000o =o 4,300o𝑙𝑏/𝑖𝑛.
𝐿 100(
=


Naturalofrequency:
0o𝑘 4300o×o386
𝜔o = =o0 =o 23.52o𝑟𝑎𝑑/𝑠𝑒𝑐
𝑚o 3000

Freeovibrationoresponseoofoundampedooscillator:
𝑢Oo
𝑢(𝑡)o =o 𝑢O 𝑐𝑜𝑠𝜔𝑡o+o 𝑠𝑖𝑛𝜔𝑡
𝜔


2

, 𝑢(𝑡)o =o −𝑢O𝜔𝑠𝑖𝑛𝜔𝑡o +o𝑢O𝑐𝑜𝑠𝜔𝑡

Displacementoandovelocityoato𝑡o =o 1𝑠𝑒𝑐owithotheoinitialovalues

𝑢Oo =o 1o𝑖𝑛.o,o𝑢Oo =o 20o𝑖𝑛./𝑠𝑒𝑐:
20
𝑢(1)o =o 1o∙o𝑐𝑜𝑠(23.5o∙o1)o+o 𝑠𝑖𝑛(23.5o∙o1)o =o −0.89o𝑖𝑛.
23.5
𝑢(1)o =o −1o∙o23.5𝑠𝑖𝑛(23.5o∙o1)o+o20𝑐𝑜𝑠(23.5o∙o1)o =o 22.66o𝑖𝑛./𝑠𝑒𝑐




1.3

Theostiffnessoofotheobeamois


12𝐸𝐼W 3𝐸(2𝐼X) 12o∙o(30o∙o10Z)o∙o170.9 3o∙o(30o∙o10Z)o∙o82.5
𝑘o = o V o o ( + Yo= + =o 25,577o𝑙𝑏/𝑖𝑛.
𝐿 𝐿( 144( 144(


Naturalofrequency:

1o 𝑘 1 25,577o×o386
0o
𝑓o = o =o 0 =o2.24o𝑐𝑝𝑠
2𝜋 𝑚o 2𝜋o 50,000




1.4

a) Infinitelyorigidohorizontalomember

Stiffness:
o




12𝐸𝐼 12o∙o(30o∙o10Z)o∙o171
𝑘o =o 2o#o (o ,o= =o 21,100o𝑙𝑏/𝑖𝑛.
𝐿 (12o∙o15)(


Naturalofrequency:



3

, 0o𝑘 21,100o×o386
𝜔o = =o0 =o 18.05o𝑟𝑎𝑑/𝑠𝑒𝑐
𝑚o 25,000
𝜔
𝑓o =o =o 2.87o𝑐𝑝𝑠
2𝜋

b) FlexibleohorizontalomemberoconsistingoofoW18X30

Computeotheostiffnessobyomomentodistributionomethod.oDisplaceotheoframeohorizontallyobyo
oneoinchoandodetermineotheostiffnessoofotheoframeoasotheosumoofotheoshearoforcesoinobothocol
umns.oTakeoadvantageoofotheosymmetryobyomodifyingotheostiffnessoofohorizontalomemberobyo
factoro3/2.


Distributionofactors
4𝐸𝐼o 4𝐸o
𝑘 =o =o ∙o171o →o 171o →o 0.1244
^_
𝐿 𝐿
4𝐸𝐼o3o 4𝐸o o 3
𝑘 =o =o ∙ ∙o802o →o 1203o →o 0.8756
^a
𝐿o 2 𝐿o 2o


Fixedoendomoments:
0.1244 0.8756
C
950 B
6𝐸𝐼o 6o∙o(30o∙o10Z)o∙o170.9
𝑀 =o 𝑀 =o = -118 -832
^_ _^ 𝐿X (12o∙o15)X o o -832o

832
=o 950o(𝑘o−o𝑖𝑛.o)

Shearoforce:
832o+o891o
𝑘o =o ∙o2o =o 19.14o𝑘𝑖𝑝/𝑖𝑛.
180 950 A D
-59
Naturalofrequency:
891

1o
𝑘 1 19,140o×o386
0o =o 0
𝑓o = o =o 2.74o𝑐𝑝𝑠
2𝜋 𝑚o 2𝜋o 25,000



Note:
1. Assumingoaoflexibleogirderodecreasesotheonaturalofrequencyobyoonly


4

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Institution
Structural Dynamics Theory and Computation
Course
Structural Dynamics Theory and Computation

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Number of pages
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