Docsity
Docsity

Prepare for your exams
Prepare for your exams

Study with the several resources on Docsity


Earn points to download
Earn points to download

Earn points by helping other students or get them with a premium plan


Guidelines and tips
Guidelines and tips

Atmospheric Boundary Layers and Turbulence - Wind Engineering - Lecture Slides, Slides of Environmental Law and Policy

Some concept of Wind Engineering are Aeroelastic Effects, Along-Wind Dynamic Response, Antennas and Open-Frame Structures, Atmospheric Boundary Layers and Turbulence, Atmospheric Boundary, Basic Bluff-Body Aerodynamics. Main points of this lecture are: Atmospheric Boundary Layers and Turbulence, Layers and Turbulence, Turbulence, Topography, Change of Terrain, Atmospheric Boundary, Gust Factors, Gust Speeds, Ratio of the Maximum, Density Function

Typology: Slides

2012/2013

Uploaded on 04/25/2013

gurudev
gurudev 🇮🇳

4.6

(10)

102 documents

1 / 23

Toggle sidebar

This page cannot be seen from the preview

Don't miss anything!

bg1
Atmospheric boundary layers and
turbulence II
Docsity.com
pf3
pf4
pf5
pf8
pf9
pfa
pfd
pfe
pff
pf12
pf13
pf14
pf15
pf16
pf17

Partial preview of the text

Download Atmospheric Boundary Layers and Turbulence - Wind Engineering - Lecture Slides and more Slides Environmental Law and Policy in PDF only on Docsity!

Atmospheric boundary layers and

turbulence II

  • Topics :
    • Turbulence (Section 3.3 in book)
    • gust factors, spectra, correlations
    • Effect of topography (Section 3.4 in book)
    • Change of terrain (Section 3.5 in book)

Gust speeds and gust factors :

  • Gust factor, G, is the ratio of the maximum gust speed to the mean wind speed :

At 10 metres height in open country, G  1.45 ( higher latitude gales)

In hurricanes, G  1.55 to 1.

U

G 

Wind spectra :

As discussed in Lecture 5, the spectral density function provides a description of the frequency content of wind velocity fluctuations

Empirical forms based on full scale measurements have been proposed for all 3 velocity components

These are usually expressed in a non-dimensional form, e.g. :

2 u

u

n.S (n)

Sometimes u*^2 orU^2 is used in the denominator

Wind spectra :

von Karman spectrum :

at high frequencies, n.Su(n)  n-2/3, or Su(n)  n-5/

2 2 5 / 6 1 70. 8

4

. ( )

 

 

 

  

  

 

 

  

 

U

n

U

n nS n

u

u

u

u l

l

at zero frequencies, Su(0)  4 u^2 lu /U

The latter is a property of turbulence in a frequency range known as the inertial sub-range

Wind spectra :

zero frequency limit :

(von Karman spectrum satisfies this)

From Lecture 5 : 

 

2 n

Su (n) 2 u( )e dτ

  i ^ 

 (^) 

Su (n)  4 0  u( )e i^2 n^ dτ

since auto-correlation is a symmetrical function of  : u(-) = u()

 (^)  Su (n)  4  (^) u^20 R u( )e i^2 n^ dτ

 Su (0)  4  (^) u^20 R u( )dτ^ setting n = 0

1

2

Su (0) 4 σu T T 1 is time scale (Lecture 5)

S u (0) 4 σu^2 lu/U

Busch and Panofsky spectrum for vertical component w(t):

Length scale in this case is height above ground, z Maximum value of 0.258 occurs at n.z/U of 0.

 

 

 

  

  

 

 

  

 2 ^ 5/ w

w

U

1 11.16 nz

U

2.15 nz σ

n.S (n)

0.01 0.10 1.00 10.

Busch & Panofsky

n.Sw(n)/ w^2

n.z / U

Co-spectrum of longitudinal velocity component :

As discussed in Lecture 5, the normalized co-spectrum represents a frequency-dependent correlation coefficient :

It is important use is to determine the strength of wind forces at the natural frequency of a structure, and hence the resonant response

Exponential decay function :

As separation distance z increases, or frequency, n, decreases, co-spectrum (z,n) decreases

 

  

  

  

    U

k.n. z ρ(Δz,n) exp

Disadvantages : 1) goes to 1 as n0, even for very large z

  1. does not allow negative values

Effects of topography :

Shallow topography : no separation of flow (follows contours)

Predictable from computer models, wind-tunnel models

shallow escarpment

shallow hill or ridge

Effects of topography :

Steep topography : separation of flow occurs

Less predictable from computer models, wind-tunnel models OK at large enough scale

steep escarpment

separation

steep escarpment

steep hill or ridge

separation separation

Topographic multiplier :

denoted by Mt : (^) :

Can be greater or less than 1. Codes only give values > 1

Wind speed at height z abovethe flat groundupwind

Wind speed at height z abovethe feature Topographic Multiplier , ,

, , 

Mt for mean wind speeds

Mˆ t for peak gust wind speeds (^) :

ASCE-7 : Kz,t = (1 + K 1 K 2 K 3 )^2 Mt = 1 + K 1 K 2 K 3

Shallow hills :

 is the upwind slope = H/2Lu

k is a constant for a given type of topography

s is a position factor

Mt  1  ks

Lu

H /

crest

= 1.0 at crest <1 upwind and downwind, and with increasing height

Shallow topography : Gust multiplier :

Assume that standard deviation of longitudinal turbulence, u, is unchanged as the wind flow passes over the hill

Mˆ^ t  1 ks

u

t u t (^) U gσ

U.M gσ Mˆ 

u

u U gσ

U.(1 ks ) gσ 

u

u

u

U gσ

U

1 gσ

ks (U gσ ). 1

U

1 gσ

ks 1 u

U

1 gσ

k in which, k  u

Steep topography :

Can be treated approximately by taking an effective slope, ' = 0.

then same formulae are used, i.e. :

Mt  1 ksυ

Mˆ^ t  1 ksυ

However these formulae are less accurate than those for shallow hills and do not account for separations at crest of escarpment or on lee side of a hill or ridge