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Calculating Influence Coefficients & Mean Components for Static & Background Loads, Slides of Environmental Law and Policy

An in-depth analysis of effective static loading distributions, focusing on the calculation of influence coefficients and mean components for both static and background loads. The concept of effective static loading distributions, the influence coefficient, and its relationship to load effects such as bending moment and shear. It also includes formulas for calculating the mean component of a load effect and the background component, as well as the correlation coefficient between the fluctuating load effect and the fluctuating pressure at a specific position. Useful for students and professionals in civil engineering, mechanical engineering, and related fields.

Typology: Slides

2012/2013

Uploaded on 04/25/2013

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Effective static loading

distributions

  • Static load distributions which give correct peak load effects under

fluctuating wind loading

Separately calculate e.s.l.d  s for :

  • mean component
  • background component
  • resonant components
  • Generally e.s.l.d. s depend on load effect (e.g. bending moment, shear)

Influence coefficient :

Value of a load effect as a unit load is moved around a structure :

Influence coefficient :

Value of a load effect as a unit load is moved around a structure :

Influence coefficient :

Value of a load effect as a unit load is moved around a structure :

Influence coefficient :

Value of a load effect as a unit load is moved around a structure :

Influence line - Central B.M.

-0.

0

0 0.2 0.4 0.6 0.8 1

position/total beam length

Influence coefficient :

Value of a load effect as a unit load is moved around a structure :

Influence line - Central B.M.

-0.

0

0 0.2 0.4 0.6 0.8 1

position/total beam length

Influence coefficient :

Value of a load effect as a unit load is moved around a structure :

Influence line - Central B.M.

-0.

0

0 0.2 0.4 0.6 0.8 1

position/total beam length

Influence coefficient :

Value of a load effect as a unit load is moved around a structure :

Influence line - Central B.M.

-0.

0

0 0.2 0.4 0.6 0.8 1

position/total beam length

Ir(z) z

For a distributed load p(z) , r =

L

0

p(z)Ir (z) dz

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Mean component

 p(z) = [0.5 aUh^2 ] Cp

on a tower :  f (z) = [0.5 a  U(z)^2 ] Cd

b(z) (per unit height)

Background (quasi-static) component

Consider a load effect r with influence line Ir(z):

Instantaneous value of r : r(t) = 

L

0

p(z,t) Ir (z) dz

p(z,t) = fluctuating pressure at z

L is length of the structure

Mean value of r : 

L

0

r p(z) Ir (z) dz

Background (quasi-static) component

Standard deviation of r :

(background) (Lecture 9)

Expected maximum value of r :

Distribution for maximum response : pB(z) = gB pr (z) p (z)

L^1 /^2

0

1 2 r 1 r 2 1 2

L

0

σ (^) r,B p(z )p(z ) I (z ) I (z ) dzdz  

 (^)    

rˆ^ rgBσr,B

p r,B

L

0

1 r 1 1

pr σ (z) σ

p(z,t) p(z ,t) I (z ) dz

ρ (z)

  

 p r,B

1 r 1 1

L

0 σ (z) σ

p (z,t)p(z ,t)I (z ) dz

Background (quasi-static) component

Discrete form of pr :  (^) i k k  (^) pi r k

ρr, (^) pi p (t)p (t)I σ σ

This form is useful when using using wind-tunnel data obtained

from area-averaging over discrete measurement panels

k

I

i

(t)I

k

2 p (t)p

r

i k i

Standard deviation of load effect :  

Example (pitched free roof) :

(Appendix F in book)

2 1

22.5

h