Single-Degree-of-Freedom (SDOF) and Response Spectrum

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1 Single-Degree-of-Freedom (SDOF) and Response Spectrum Ahmed Elgamal 1 Dynamics of a Simple Structure The Single-Degree-Of-Freedom (SDOF) Equation References Dynamics of Structures, Anil K. Chopra, Prentice Hall, New Jersey, ISBN (Chapter 3). Elements of Earthquake Engineering And Structural Dynamics, André Filiatrault, Polytechnic International Press, Montréal, Canada, ISBN (Section 4..3). 1

2 Equation of motion (external force) Free-Body Diagram (FBD) f I p(t) f S f D f s f D f I + f D + f s = p(t) where f I,f D, and f s are forces due to Inertia, Damping and Stiffness respectively: m u cu ku p(t) k 1 f s = k u u c 1 f D = c ů ů c m u (t) p(t) f D f S f I p(t) k FBD Mass-spring damper system 3 Earthquake Ground Motion (u g ) f I + f D + f s = 0 f I = m u = m(u u t m(u u g ) cu ku 0 mu cu ku mu g g ) You may note that: u g (t) = (t) External force Earthquake Excitation u g (t) Fixed base u = relative displacement (displacement of the structure relative to the ground) u t = total displacement f I = m x (total or absolute acceleration) 4

3 Undamped natural frequency Property of structure when allowed to vibrate freely without external excitation k m Undamped natural circular frequency of vibration (radians/second) f natural cyclic frequency of vibration (cycles/second or 1/second or Hz) 1 T natural period of vibration (second) f T is the time required for one cycle of free vibration T If damping is present, replace by D where D 1 natural frequency*, and c m c c c fraction of critical damping coefficient (damping ratio, zeta) c (dimensionless measure of damping) km c c m km c c = critical damping * Note: In earthquake engineering, D = approximately, since is usually below 0. (or 0%) 5 cin c is general the least level < 0., of i.e., damping D that, fprevents D f, T = oscillation T D u In c c general least damping < 0., that i.e., prevents D, oscillation f D f, T = T D c c or larger 1 may be in the range of or % - 0% 5% is sometimes a typical value. e.g., damper on a swinging door t in terms of mu cu ku mu g u c m u k u m u g u u u u g 6 3

4 Note: After the phase of forced vibration (due to external force or base excitation, or initial conditions), the structure continues to vibrate in a free vibration mode till it stops due to damping. The ratio between amplitude in two successive cycles is ui e ui1 where we define the logarithmic decrement as u i ln if you measure a free vibration response you can find. u i1 Note: for peaks j cycles apart u i u i+1 u ln i j j ui j Free vibration 7 Why is c c m km Critical viscous damping The free vibration equation may be written as m x cx kx 0 and the general solution is c m x C1 e c k m m t C c m e c k m m t c if m k m, the radical part of the exponent will vanish. This will produce aperiodic response (non-oscillatory). In this case c k or c km c c (m) m k since, c c is also equal to m (note that km m m m ) m k and also cc km k(k / ) 8 4

5 mw k1(w u1g ) k (w u g ) 0 mw (k1 k )w k1u1g kug c c c (0.05 for example) cc (k1 k )m if u1g ug ug mw (k1 k)w (k1 k) u but w = u + u g g m u(k1 k)ug (k1 k)u mu g (k1 k) ug or m u (k1 k)u m u g 9 First version: 003 (Last modified 010) 10 5

6 First version: 003 (Last modified 010) 11 Deformation Response Spectrum For a given EQ excitation calculate u max from SDOF response with a certain and within a range of natural periods or frequencies. u max for each frequency will be found from the computed u(t) history at this frequency. A plot of u max vs. natural period is constructed representing the deformation (or displacement) response spectrum (S d ). From this figure, one can directly read the maximum relative displacement of any structure of natural period T (and a particular value of as damping) From: Chopra, Dynamics of Structures, A Primer 1 6

7 First version: 003 (Last modified 010) Example Units for natural frequency calculation (SI units) Weight = 9.81 kn = 9810 N = 9810 kg (m /s ) Gravity (g) = 9.81m/s Mass (m) = W/g = 9180/9.81 = 1000 kg Stiffness (k) = 81 kn/m = N/m = kg (m/s )/m = kg /s = SQRT (k/m) = SQRT (81000/1000) = 9 radians/sec f = / ( ) = 1.43 Hz (units of 1/s or cycles/sec) Units for natural frequency calculation (English units) Weight (W) = 193. Tons = 193. (000) = 386,400 lbs = kips g = in/sec/sec (or in/s ) Mass (m) = W/g = 1.0 kips s /in Stiffness (k) = 144 kips/in =SQRT (k/m) = 1 radians/sec f = / ( ) = 1.91 Hz (units of 1/s or cycles/sec) Note: The weight of an object is the force of gravity on the object and may be defined as the mass times the acceleration of gravity, w = mg. Weight is what is measured by a scale (e.g., weight of a person). Since the weight is a force, its SI unit is Newton. 13 Concept of Equivalent lateral force f s If f s is applied as a static force, it would cause the deformation u. Thus at any instant of time: f s = ku(t), or in terms of the mass f s (t) = m u(t) The maximum force will be fs,max m u max ku max msa ksd k Sa S d m Sa Sd k m S d = deformation or displacement response spectrum Sa Sd = pseudo-acceleration response spectrum The maximum strain energy E max stored in the structure during shaking is: E max 1 ku max where Sv S d 1 ks d 1 k ω S ω d 1 mω S d = pseudo-velocity response spectrum 1 ms V From: Chopra, Dynamics of Structures, A Primer 14 7

8 Note that S d, S v and S a are inter-related by Sa Sd Sv S a, S v are directly related to S d by and respectively or by (f) and f; or and as shown in Figure. T T Due to this direct relation, a 4-way plot is usually used to display S a, S v and S d on a single graph as shown in Figure. In this figure, the logarithm of period T, S a, S v and S d is used. From: Chopra, Dynamics of Structures, A Primer 15 From: Chopra, Dynamics of Structures 16 8

9 In order to cover the damping range of interest, it is common to perform the same calculations for =0.0, 0.0, 0.05, 0.10, and 0.0 (see Figure) Typical Notation: S v PSV V S a PSA A S d SD D Example (El-Centro motion): Find maximum displacement and base shear of tower with f = Hz, = % and k = 1.5 MN/m Period T = 1/f = 0.5 second S d =.5 inches = m Force max = ku max = 1.5 MN/m x m = 95.5 kn From: Chopra, Dynamics of Structures, A Primer 17 First version: 003 (Last modified 010) 18 9

10 September 003 (5% Damping) 19 September

11 Inspection of this figure shows that the maximum response at short period (high frequency stiff structure) is controlled by the ground acceleration, low frequency (long period) by ground displacement, and intermediate period by ground velocity. Get copy of El-Centro (May 18, 1940) earthquake record S00E (N-S component) ftp nisee.ce.berkeley.edu ( ) login: anonymous password: your_indent cd pub/a.k.chopra get el_centro.data quit From: Chopra, Dynamics of Structures 1 Note that response spectrum for relative velocity may be obtained from the SDOF response history, and similarly for ü t =(ü+ü g ). These spectra are known as relative velocity and total acceleration response spectra, and are different from the pseudo velocity and pseudo acceleration spectra S v and S a (which are directly related to S d ). e.g. for = 0% m(ü+ü g ) + ku = 0 or (ü+ü g ) + u = 0 From: Chopra, Dynamics of Structures 11

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19 Elastic Design Spectrum Use recorded ground motions (available) Use ground motions recorded at similar sites: Magnitude of earthquake Distance of site form earthquake fault Fault mechanism Local Soil Conditions Geology/travel path of seismic waves From: Chopra, Dynamics of Structures Motions recorded at the same location. For design, we need an envelope. One way is to take the average (mean) of these values (use statistics to define curves for mean and standard deviation, see next page) 37 From: Chopra, Dynamics of Structures The response spectra used to derive this design spectrum would typically share common characteristics of relevance to the geographic location of interest such as: distance from causative fault, soil profile at the site, expected earthquake magnitude, fault rupture mechanism, and so forth,.. Mean response spectrum is smooth relative to any of the original contributing spectra 38 19

20 As an alternative Empirical approach, the periods shown on the this Figure and the values in the Table can be used to construct a Median elastic design spectrum (or a Median + one Sigma), where Sigma is the Standard Deviation. For any geographic location, these spectra are built based on an estimate of peak ground acceleration, velocity, and displacement as this location. From: Chopra, Dynamics of Structures The periods and values in Table were selected to give a good match to a statistical curve such as Figure 6.9. based on an ensemble of 50 earthquakes on competent soils. 39 First version: 003 (Last modified 010) (Design Spectrum may include more than one Earthquake fault scenario) About Caltrans ARS Online This web-based tool calculates both deterministic and probabilistic acceleration response spectra for any location in California based on criteria provided in Appendix B of Caltrans Seismic Design Criteria 40 0

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