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F. K. Kong MA, MSc, PhD, CEng, FICE, FIStructE, R. H. Evans CBE, DSc, D ès Sc, DTech, PhD, CEng, FICE, FIMechE, FIStructE (auth.)-Reinforced and Prestressed Concrete-Springer US (1987)

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Problems 289

refers to a particular initial crookedness e0 = e1 sinHzll. However, any

arbitrary initial crookedness may be represented by a Fourier series:

. Hz . 2Jr:z . 3Hz

e0 = e1siDT + e2 siD- 1 - + e3 siD- 1 - + · · ·

Using the same technique that you used for Problem 7.6, show that for this

general case the total transverse deflection is

e1 . HZ e2 . 2Jr:z

eo+ eadd = 1- aESIDT + 1- (aE/22)siD-le3

. 3Hz en . nHz

+ 1 - (aE/32)siD-l- + · · · 1- (aE/n2)siD-l- +

Comments on Problem 7.7 (May be omitted during first reading)

(a) The Fourier series solution is of wide application, as illustrated by the

following two examples.

First, consider an eccentrically loaded column (Fig. 7.4-3). The

eccentricity e may be thought of as an initial crookedness of uniform

magnitude ( = e) along the entire column length, and represented by a

Fourier series. The result of Problem 7. 7 becomes directly applicable.

Next consider a column subjected to an axial load N and end

moments Mi (Fig. 7.4-1(a)). The transverse deflection e 0 due to Mi

acting alone is of course easily calculated. The total transverse

deflection due to N and Mi may then be determined by considering

the load N acting (in the absence of Mi) on a column having an initial

crookedness e 0 . By expressing e 0 as a Fourier series, the result of

Problem 7. 7 becomes directly applicable:

"' en . nHZ

eo + eadd = LJ 1 _ (aE/n2) SID -~-

Note that (e0 + eadd) here has the same meaning as eadd in Fig.

7.4-1(a).

(b) The Fourier series solution for e0 + eadd tends to converge rapidly. In

many practical applications, a good estimate is obtained by just

taking the first term:

el . HZ

eo + eadd = 1 SID -1

- aE

e1 I

= 1 - . aE

at z = - 2

Therefore, referring to Fig. 7.4-1(a), the total moment is,

approximately:

M = M· + Net

t • 1- aE

Interested readers are referred to Section 9.4 of Reference 6, which

shows that this simple equation forms the basis of the well-known

Perry-Robertson formula in structural steelwork design:

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