Section 2 Aerodynamic data
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Clasifications Register Rules and Regulations - Rules and Regulations for the Classification of Linkspans, July 2022 - Part 3 Construction, Design and Test Requirements - Chapter 9 Highway Loads, Section Aerodynamics and Pontoon Drag Coefficients - Section 2 Aerodynamic data

Section 2 Aerodynamic data

2.1 Wind force coefficient, C f

2.1.1 The force coefficient for various structural components is given in Table 9.2.1 Force coefficient (Cf). The values for individual members vary according to the aerodynamic slenderness and in the case of large box sections, with the section ratio.

Table 9.2.1 Force coefficient (Cf)

Type Description Aerodynamic slenderness l/b or l/D
5 10 20 30 40 50
Force coefficient C f
Individual members Rolled sections, rectangles, hollow sections, flat plates, box section with b or d less than 0,5m 1,30 1,35 1,60 1,65 1,70 1,80
Circular section, where DV s < 6,0 m2/s 0,75 0,80 0,90 0,95 1,00 1,10
  DV s ≥ 6,0 m2/s 0,6 0,65 0,70 0,70 0,75 0,80
    b/d            
Box section with b or d greater than 0,5 m ≥ 2,00 1,55 1,75 1,95 2,10 2,20  
    1,00 1,40 1,55 1,75 1,85 1,90  
    0,50 1,00 1,20 1,30 1,35 1,40  
    0,25 0,80 0,90 0,90 1,00 1,00  
Single lattice frames Flat sided sections 1,70
Circular section, where DV s < 6,0 m2/s 1,20
  DV s ≥ 6,0 m2/s 0,80
Machinery houses, etc. Rectangular clad structures on ground or solid base (air flow beneath structure prevented) 1,10
D = the diameter of the section, in metres
V s = the design wind speed, in m/s

2.2 Aerodynamic slenderness and section ratio

2.2.1 The aerodynamic slenderness and section ratio are defined in Figure 9.2.1 Aerodynamic slenderness and section ratio.

Figure 9.2.1 Aerodynamic slenderness and section ratio

2.3 Shielding and solidity factors

2.3.1 Where a structure consists of a framework of members such that shielding takes place, the wind force on the windward frame or member and on the sheltered parts of those behind it is calculated using the appropriate force coefficient. The force coefficient on the sheltered parts is to be multiplied by a shielding factor η. The values of η vary with the solidity and spacing ratio of the framework. Values of η are given in Table 9.2.2 Shielding factor(n) for the solidity and spacing ratio as defined in Figure 9.2.2 Solidity ratio and spacing ratio.

Figure 9.2.2 Solidity ratio and spacing ratio

Table 9.2.2 Shielding factor(n)

Spacing ratio Solidity ratio A/A e
a/b 0,1 0,2 0,3 0,4 0,5 0,6
0,5 0,75 0,4 0,32 0,21 0,15 0,1
1,0 0,92 0,75 0,59 0,43 0,25 0,1
2,0 0,95 0,8 0,63 0,5 0,33 0,2
4,0 1 0,88 0,75 0,66 0,55 0,45
5,0 1 0,95 0,88 0,81 0,75 0,68
6,0 1 1 1 1 1 1

2.3.2 Where a structure consists of a number of identical frames or members spaced equidistantly behind each other in such a way that each frame shields those behind it, the wind load is to be obtained from the following expression:

where
η = shielding factor from Table 9.2.2 Shielding factor(n) but to be taken as not less than 0,1
n = number of frames, but to be taken as not greater than nine
C f = force coefficient from Table 9.2.1 Force coefficient (Cf)

and A and P are as defined in Pt 3, Ch 3, 3.6 Wind loading 3.6.3.

2.4 Tower sections

2.4.1 For latticed tower structures, the `face on' wind force based on the solid area of the windward face is to be calculated using the following factored pressures:

  1. For towers composed of flat-sided sections:

  2. For towers composed of circular sections:

    where

    and

    where
    = D and V s are defined in Table 9.2.1 Force coefficient (Cf).

The value of η is taken from Table 9.2.2 Shielding factor(n) for a/b = 1,0 according to the solidity ratio of the windward face.

2.4.2 The maximum wind load on a square section tower occurs when the wind blows on to a corner and is to be taken as 1,2 times the `face on' load.


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