Exam Flashcards

(37 cards)

1
Q

Phase angle = 180 degrees

A

completely out of phase

  • w / wn&raquo_space; 1
  • high frequency response
  • small amplitude
  • force rapidly changing
  • response controlled by mass of system
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2
Q

Phase angle = 90 degrees

A

resonance: w = wn
large amplitude
- Rd very sensitive to damping
- response controlled by damping

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3
Q

phase angle = 0 degrees

A

in phase

  • w / wn &laquo_space;1
  • low frequency response
  • quasistatic response u0 = p0/k
  • force slowly varying
  • amplitude of dynamic response controlled by stiffness of system
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4
Q

Ritz vectors

A
  • used to find approximate natural frequencies

- use estimated vectors of mode shaped based on good judgement

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5
Q

earthquake: max strain energy

A

= 1/2 m v^2

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6
Q

earthquake: max force

A

= mA

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7
Q

fundamental assumption in earthquake response analysis:

A

structures subjected to a random motion tend to vibrate at various amplitudes but with a frequency very near to lowest natural frequency
e.g. the sinusoidal relationshp A = wn D is approximately valid

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8
Q

convergence

A

means that the solution tends towards the exact solution as the time step becomes smaller

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9
Q

stability

A

means that the algorithm is stable in relation to small disturbances such as round of errors and does not diverge due to these disturbances

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10
Q

unconditionally stable

A
  • Newmark’s method - average acceleration special case

- gamma = 0.5, beta = 0.25

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11
Q

Requirements of time-stepping procedures

A

1) convergence
2) stability to round of errors
3) accuracy and efficiency

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12
Q

classical damping

A

if C is diagonalisable

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13
Q

Rayleigh Damping

A

C = alpha m + beta k
(alpha and beta constants)
- classical damping

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14
Q

Modal Damping

A

each mode can be assigned a damping ratio

- c is a sum of matrices found by “expanding” the mode vectors

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15
Q

impulse

A

I = m v(0)

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16
Q

Response spectrum

A

shows the maximum response (D,V,A) for a spectrum of buildings in terms of (wn, damping) subjected to a particular earthquake

17
Q

Design Spectrum

A

an idealised maximum response for a large number of (historic or synthetic) earthquakes - the envelope of responses

18
Q

wn relationship to fn

A

wn = 2 * pi * fn

19
Q

fn relationship to Tn

20
Q

Requirements in designing isolators

A
  • Stiffness
  • Isolation
  • Damping
21
Q

Essential properties of rubber

A
  • Elasticity
  • Damping
  • Incompressibility
  • isotropy
  • rate and amplitude dependance
  • temperature dependance
  • damage effects
22
Q

Essential properties of shock absorbers

A
  • spring characteristic
  • deformation behaviour
  • strain energy capacity
  • fatigue sensitivity
23
Q

material make up of carbon black filled rubber

A
  • crosslinks (give rubber part of its elasticity)
  • polymer chains
  • carbon black (soot)
    helps to make much stiffer material
24
Q

pulse loading : td &laquo_space;Tn

A

impulse
I = integral ( p(t) dt ) = m v(0)

u(0) = I / (m * wn)

25
pulse loading td >> Tn
quasi-static | u(0) = p(0) / k
26
Shock absorption energy
W = deltaT W = integral(F dx) = Fmean * dx deltaT = 1/2 m v(0)^2
27
Fmean (shock absorption)
Fmean = m * v(0) ^ 2 / (2 * delta(x) )
28
Shock absorption: impulse and momentum
I = deltaG I = integral Fdt = Fmean dt deltaG = mv(0)
29
deltat (shock absorption)
delta(t) = m * v(0) / Fmean
30
TR
TR = f(t0) / p(0) where f(t0) = k * u(0)
31
Reduction methods
- Static condensation - Modal Truncation - Generalised SDOF system - Rayleigh-Ritz method
32
Static condensation
DOFs without inertia are eliminated (partitioned system)
33
Modal Truncation
higher modes neglected in modal expansion | - approximation good if spatial distribution of external forces triggers lower modes
34
Generalised SDOF system
approximation of first mode to obtain SDOF system | - useful for determining the lowest natural frequency
35
Approximation by Ritz Vectors
special set of base vectors to express the displacements Choice of vectors can be based on: 1) physical insight 2) an automatic procedure giving Ritz vectors that conform with the spatial distribution of the load
36
non-classical damping
C is not able to be diagonalised (by premultiplying with Phi transpose)
37
Construction of Classical Damping Ratios
1) Rayleigh Damping | 2) Superposition of modal damping matrices