openings in beams

57
Assoc Prof Tan Kiang Hwee Department of Civil Engineering National University of Singapore CE5510 Advanced Structural Concrete Design - Design & Detailing of Openings in RC Flexural Members-

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Page 1: Openings in Beams

Assoc Prof Tan Kiang HweeDepartment of Civil EngineeringNational University of Singapore

CE5510 Advanced Structural Concrete Design

- Design & Detailing of Openings

in RC Flexural Members-

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DEPARTMENT OF CIVIL ENGINEERING

Tan K H, NUSA/P Tan K H, NUS A/P Tan K H, NUS 2

In this lecture

We will explore

!Types of openings!Behaviour of beams with large

openings!Design for ultimate strength!Crack Control!Deflection Calculation

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DEPARTMENT OF CIVIL ENGINEERING

Tan K H, NUSA/P Tan K H, NUS A/P Tan K H, NUS 3

At the end of the lecture

You should be able to

!Understand the behaviour of beams with openings under bending and shear

!Design the opening using Mechanism Approach, Plasticity Truss Method or Strut-and-Tie Method

!Detail the reinforcement to satisfy serviceability and ultimate limit states

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NationalUniversity

ofSingapore

© Tan KH NUS

Beams with Openings: and Design.Mansur, M.A. and Kiang-Hwee Tan.CRC Press Ltd, 1999

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DEPARTMENT OF CIVIL ENGINEERING

Tan K H, NUSA/P Tan K H, NUS A/P Tan K H, NUS 5

Additional references

! Mansur, M.A., Tan, K.H. and Lee, S.L., "A Design Method for Reinforced Concrete Beams with Large Openings", Journal of the American Concrete Institute, Proceedings, Vol. 82, No. 4, USA, July/August 1985, pp. 517-524.

! Tan, K.H. and Mansur, M.A., "Design Procedure for Reinforced Concrete Beams with Web Openings", ACI Structural Journal, Vol. 93, No. 4, USA, July-August 1996, pp. 404-411.

! Mansur, M.A., Huang, L.M., Tan, K.H. and Lee, S.L., "Analysis and Design of R/C Beams with Large Web Openings", Journal of the Institution of Engineers, Singapore, Vol. 31, No. 4, July/August 1991, pp. 59-67.

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Opening in beam

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Classification of Openings" By geometry:

– Small opening ifDepth or diameter ≤ 0.25 x beam depthand Length ≤ depth

– Large opening otherwise.

h≤ 0.25hd ≤ 0.25h

≤ d

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" By structural response:

– Small opening ifBeam-type behaviour persists.

– Large opening otherwise.

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TS T2

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DESIGN TOOLS" Finite element analysis:

• elastic stress state• area of stress concentration

" Truss analysis (Strut-and-tie model):• lower bound approach• detailing for crack control and strength

" Tests:• specific cases• serviceability & strength aspects

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BEHAVIOUR ofBEAMS WITH LARGE OPENINGS

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Principaltensionstress

contours

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Mt +Mb + Nz = M= MNt + Nb = 0Vt + Vb = V

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Inadequately reinforced openings

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actual

idealised

33

2

2

1

1

44

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Shear carried by chords

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Contra-flexural points

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DESIGN & DETAILINGof OPENINGS - General guidelines

• sufficient area to develop ultimate compression block in flexure

• openings to be located more than D/2from supports, concentrated loads and adjacent openings

• opening depth ≤≤≤≤ D/2• opening length

• stability of chord member• deflection requirement of beam

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" Crack control

• principal tensile stress direction• stress concentration• congestion of reinforcement

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⇒shear concentration factor of 2 (i.e. 2Vu)⇒diagonal bars to carry 50~75% of total

shear; vertical stirrups to carry the rest

2

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" Strength requirement– 2 general approaches:

• mechanism approach◊ failure at an opening is due to the

formation of four plastic hinges, one at each corner of the opening

• truss model approach◊ plasticity truss method◊ strut-and-tie method◊ applied loads are transferred across

opening to supports by a truss system◊ lower bound approaches

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Mechanism Approach

" Rigorous method

1. Calculate Mu and Vu at centre of opening.

2. Assume suitable reinft. for chord members.

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3. Determine Nu in chord members and hinge moments (Mu)*,* from

Nu = [Mu - (Ms)t - (Ms)b]/z

where(Ms)t = [(Mu)t,1 +(Mu)t,2]/2(Ms)b = [(Mu)b,4 +(Mu)b,3]/2

and (Mu)*,* are related to Nu by the respective M-N interaction diagrams.

Slide 15

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4. Calculate Vu in chord members from

(Vu)t = [(Mu)t,2 - (Mu)t,1]/llll(Vu)b = [(Mu)b,4 - (Mu)b,3]/llll

where llll is the opening length.

5. Check that (Vu)t+(Vu)b ≅≅≅≅ Vu.

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" Simplified method– Unknowns: Nt, Nb, Mt, Mb, Vt, Vb

– 3 equations:Mt +Mb + Nz = M

Nt + Nb = 0Vt + Vb = V

⇒ Assume Mt = 0Mb = 0Vb =kVt

where k = 0k = Ab/At

or k = Ib/It

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EXAMPLEA simply supported reinforced concrete beam, 300 mm wide and 600 mm deep, contains a rectangular opening and is subjected to a series of point loads as shown. Design and detail the reinforcement for the opening if the design ultimate load Pu is 52.8 kN. Material properties are: fc’=30 MPa, fyv=250 MPa, and fy=460 MPa.

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Solution by Mechanism Approach

Assume point of contraflexure at midpoint of chord members and that 40% of shear is carried by bottom chord member.

At centre of opening,Mu = 171.6 kNmVu = 79.2 kN

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1. Bottom chord member

(Nu)b = Mu/z = 408.6 kN(Vu)b = 0.4 Vu = 31.7 kN(Mu)b =(Vu)bllll/2 = 15.1 kNm

2As = 1954 mm2

(3T20 top + 4T20 bottom)

Asv/s = 400 mm2/m (minimum)(M6 @ 100 mm spacing)

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2. Top chord member

(Nu)t=408.6 kN; (Vu)t=47.5 kN;(Mu)t=22.6 kNm

2As = 516 mm2

(2T12 +1T10 top & bottom)

Asv/s = 525 mm2/m (M6 @ 100 mm spacing)

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3T20

2T12 + 1T10

2T12 + 1T10

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Truss Model Approaches

" Plasticity truss (AIJ approach)

As

As

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" Shear capacity

Vu = 2 bdvsρρρρvfyv cot φφφφswhere

cot φφφφs = √√√√(ννννfc’/ρρρρvfyv - 1) ≤≤≤≤ 2ννννfc’/ρρρρvfyv ≥≥≥≥ 1ρρρρv = Avfyv/bsνννν = 0.7 - fc’/200

" Longitudinal reinforcement

Tsn = Asnfy = Vullll/2dvsTsf = Asffy = Vu(llll +dvs cot φφφφs )/2dvs

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Vd = Asd fyd sin θθθθd

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Solution by Plasticity Truss Method (AIJ)

1. Calculate v.v = Vu/(2bdvsννννfc’)=0.089

2. Determine shear reinforcement.From v = √ψ√ψ√ψ√ψ(1-ψψψψ), obtain

ψψψψ ≡≡≡≡ ρρρρvfyv/ννννfc’ = 0.008 →→→→ ρρρρv = 0.00053 < ρρρρv,min = 1/3fy = 0.01

Asv/s = 400 mm2/m(M6 @ 100 mm spacing)

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3. Determine longitudinal reinforcement.Asn = Vullll/2fydvs = 957 mm2

Asf = Vu(llll +dvs cot φφφφs )/2fydvs= 1080 mm2

⇒⇒⇒⇒ 3T20 (near) + 4T20 (far)

3T20

3T20

4T20

4T20

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" Strut-and-tie methodGeneral Principles

1. Idealize structure as comprising concrete struts and reinforcement ties, joined at nodes.

• follow stress path given by elastictheory; refine as necessary

• equilibrium of strut and tie forces• deformation capacity of concrete• angle between struts and ties

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2. Calculate forces in struts and ties fromequilibrium.

• check stresses in struts (< 0.6fcd)• detail reinforcement according to

calculated tie forces" check for anchorage of

reinforcement

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Solution by Strut-and-Tie Method1. Postulate strut-and-tie model.

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2. Calculate member forces.Top chord takes 91% of total shear.Stirrup force ≈≈≈≈ 3.3 times shear (Model may be simplified.)

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3. Longitudinal reinforcement.

Top chordTop steel: 1298 mm2 (4T20)Bot. steel: 1741 mm2 (4T25)

Bottom chordTop steel: 171 mm2 (2T12)Bot. steel: 590 mm2 (2T20)

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4. Transverse reinforcement.

Top chordAsv/s= 1567 mm2/m (T8 @ 65 mm)

Bottom chordAsv/s= 284 mm2/m (M6 @ 65 mm)

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A/P Tan K H, NUS 53

CALCULATION OF DEFLECTIONS

It

Ib

RigidAbutment

M-∆M M+∆MV V

∆d

ds

P P

Hinges

Stirrup

2/el 2/el

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A/P Tan K H, NUS 54

( ) I I E3

V

btc

e

+

=

3

2l

δ

Relative displacement of hinge w.r.t. one end of opening due to V(It based on gross concrete section; Ib based on a fully cracked section)

( ) ( ) ......21 +++= openingvopeningvw δδδδMidspan deflection of beam

( )I I E V

btc

ev +

==12

23lδδ

Relative displacement of one end of opening w.r.t. the other end

δVδ

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A/P Tan K H, NUS 55

Calculate the midspan service load deflection of the beam described in the Example.

SOLUTIONService load, Ps = Pu / 1.7 = 52.8 / 1.7 = 31.1 kN;

V = 1.5 Ps = 46.6 kN. Effective length of chord members, le = (950 + 50)

= 1000 mm. Assume It = Ig = 300 x 1803/12 = 146 x 106 mm4;

Ib = 0.1 x 146 x 106 mm4 ≈ 15 x 106 mm4

Also, Ec = 4730√30 = 26 x 103 MPa

Hence, δv = V le

3 / [12 Ec( It + Ib)] = 46.6 x 1012 / [12 x 26 x (146 + 15) x 109]= 0.93 mm

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A/P Tan K H, NUS 56

Midspan deflection, δw, of the beam is 11PL3/144EcI,where I can be conservatively estimated as the moment of inertia of the beam at a section through the opening. That is,

I = 2 x [300 x 1803 / 12 + 300 x 180 x 2102] = 5054 x 106 mm4

As the span L is 6 m, therefore,δw =11x 31.1 x 103 x (6000)3 / [144 x 26 x 5054 x 109]

= 3.91 mm

Hence, the total midspan deflection is calculated asδ = δv + δw = 0.93 + 3.91 = 4.84 mm

< L/360 = 16.7 mm

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Add deflection due to shear

at each opening

Deflection

Summary