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NUS structural engineering coursework lectures

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  • 12007-8-22 1

    Continuous Construction Multi-storey frames

    2007-8-22 2

    Simple Frame Design pin joints

    (a) Web Cleats (b) End Plate (c) Fin Plates

  • 22007-8-22 3

    Continuous Frame Design rigid joints

    Rigid FrameExtended end plate connection

    2007-8-22 4

    Frame design

    Braced or Unbraced

    Sway or Non-sway

    Elastic design or Plastic design

  • 32007-8-22 5

    2007-8-22 6

  • 42007-8-22 7

    Design of Independently Braced frame

    Frame B is braced by frame A if lateral stiffness is KA >4KB

    Stabilizing System to resist all horizontal load

    Independently Braced frame designed to resist gravity load only

    B A

    2007-8-22 8

    Design of independently braced frames (Cl: 5.6.2)

    Independently braced frames should be designed: to resist gravity loads (1.4DL +1.6IL). the non-sway mode effective length of the columns

    should be obtained using Annex E. pattern loading should be used to determine the most

    severe moments and forces. sub-frames may be used to reduce the number of load

    cases to be considered. the stabilizing system must be designed to resist all

    the horizontal loads applied including the notional horizontal forces. It can be sway or nonsway frame.

  • 52007-8-22 9

    Pattern Loadings : Maximum moments

    Maximum beam span moments Maximum beam support moments

    Maximum single curvature bending Maximum double curvature bendingin columns in columns

    2007-8-22 10

    Design of non-sway frames (5.6.3)

    Non-sway frames should be designed: to resist gravity loads (load combination 1). the non-sway mode effective length of the

    columns should be obtained using Annex E. pattern loading should be used to determine the

    most severe moments and forces. sub frames may be used to reduce the number of

    load cases. the frame should then be checked for

    combined vertical and horizontal loads without pattern loading.

  • 62007-8-22 11

    Design of Sway Sensitive FramesSway sensitive frames should be designed as

    follows: Check in the non-sway mode i.e. design to resist

    gravity loads (load combination 1) as for independently braced frames without taking account of sway ( i.e.without notional horizontal forces, but with pattern loading).

    * Check in the sway mode for gravity load (i.e. load combination 1) plus the notional horizontal forces without any pattern loading.

    * Check in the sway mode for combined vertical and horizontal loads (i.e. load combinations 2 and 3), without pattern loading.

    *The sway effect should be allowed for, either by using column effective lengths by using amplified sway moments.

    2007-8-22 12

    Member Buckling Check for Columns in Sway Frame

    FP

    m MZ

    m MZc

    x x

    x x

    y y

    y y+ + 10.

    Effective length for sway frame

    kampM, amplified moment or

    1ZpMm

    MMm

    PF

    yy

    yy

    b

    xLT

    cy

    c ++

    In-plane Buckling

    Lateral Torsional Buckling

  • 72007-8-22 13

    Design of Sway Sensitive FramesProvided that cr is greater than 4, the sway should be allowed for by using one of the following methods (Cl. 5.6.4):a) Effective length method.

    Use effective lengths from the sway chart of Annex E.

    b) Amplified sway method. The sway moments should be multiplied by the amplification factor kamp. LE/L is non-sway value.

    cr < 4, determine member forces by direct second-order analysis

    2007-8-22 14

    Effective lengths and critical loadsCritical load of a Pin-ended ColumnPcr = Pe = 2EI/L2Critical load of a column with other boundary

    conditionPcr = 2EI/(KL)2 = Pe/ K2KL = Effective LengthPe = Euler buckling loadEffective Length factor, K = (Pe/Pcr)0.5

    e.g., Cantilever ColumnPcr= 0.252EI/L2 = 2EI/4L2 = 2EI/(2L)2

    Effective Length factor = (Pe/Pcr)0.5Hence the effective length LE for a cantilever is 2L

  • 82007-8-22 15

    Nominal effective lengths

    None Position Position Position

    Position Position Position Position

    Direction Direction Direction

    Direction Direction Direction 1.0 L 0.85 L 0.7 L 2.0 L 1.2 L

    Position

    Restraint

    Restraint

    Practical L E

    2007-8-22 16

  • 92007-8-22 17

    2007-8-22 18

    Charts of Annex E: Effective length of columns in Nonsway frames

    KTL KTR

    Ku

    KL

    Kc

    KBRKBL

    0

    0.1

    0.2

    0.3

    0.4

    0.5

    0.6

    0.7

    0.8

    0.9

    1

    0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

    Pinned

    k 1

    Fixed

    k 2 PinnedFixed

  • 10

    2007-8-22 19

    Charts of Annex E: Effective length of columns in Sway frames

    k2

    0

    0.1

    0.2

    0.3

    0.4

    0.5

    0.6

    0.7

    0.8

    0.9

    1

    0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

    Pinned

    k 1

    Fixed

    k 2 PinnedFixed

    2007-8-22 20

    Buckled mode shapes

    Non Sway Frame Sway Frame

  • 11

    2007-8-22 21

    K

    K

    KTL

    Ku

    KTR

    KBL BR

    L

    K1

    K2

    Column being consideredK

    c= I/L

    intJoatMembersAllofStiffnessTotalintJoatStiffnessColumnTotalk =

    k k kk k k k

    c u

    c u TL TR1 = ++ + +

    k k kk k k k

    c L

    c L BL BR2 = ++ + +

    Effective Length of Columns in Multistorey Frame

    2007-8-22 22

    Derivation of Chartskl = KC / (KC + KBL + KBR)

    k2 = KC+ KL / (KC +KL + KBL + KBR)

    Conservative Formulae for the curvesFor non sway

    ( ) 22121 )(55.014.05.0/ kkkkLLE ++++

    LE

    For sway frames

    ++

    2121

    2121

    6.0)(8.0112.0)(2.01

    /kkkkkkkkLLE

    1

    2

  • 12

    2007-8-22 23

    Use of the charts of Annex E k1 = (Kc + Ku) / (Kc+Ku+KTL +KTR) k2 = (Kc + KL) / (Kc+KL+KBL +KBR) The stiffness K for each member is

    taken as a function of I / L If a beam supports a floor slab, its K

    value should be taken as I / L For a beam which is not rigidly

    connected to the column K should be taken as zero.

    2007-8-22 24

    Use of the charts of Annex E For a beam which carries more

    than 90% of its moment capacity, a pin should be inserted at that location .

    If either end of the column carries more than 90% of Mp, the value of k1 or k2 as appropriate should be taken as 1.0.

    For other conditions, the appropriate values of K are given in Tables E1, E2 and E3 of the code.

    90%Mp

    Ib/|Lb = 0

    k2 = 1

  • 13

    2007-8-22 25

    Beam stiffness values

    Loading condition

    Non-sway mode Sway mode

    Beam directly supporting concrete floor or roof slab

    1.0 ( I/L ) 1.0 ( I/L )

    Other beams supporting direct loads

    0.75 ( I/L ) 1.0 ( I/L )

    Beams with end moments only

    0.5 ( I/L ) 1.5 ( I/L )

    Table E.1 BS5950:Part1

    Non Sway Frame Sway Frame

    Beam in double curvature

    Beam in single curvature

    2007-8-22 26

    Effect of Axial Force on Beam stiffness Kb -Non sway frames

    Rotational restraint at far end of beam

    Beam stiffness coefficient Kb

    Fixed at far end 1.0 (I/L ) { 1 0.4 (Pc/PE)} Pinned at far end 0.75 (I/L ) { 1 1.0 (Pc/PE)} Rotation as at near end (double curvature)

    1.5 (I/L ) { 1 0.2 (Pc/PE)}

    Rotation equal and opposite to that at near end (single curvature)

    0.5 (I/L ) { 1 1.0 (Pc/PE)}

    Far end of the beam

    Table E.2 BS5950:Part1

    PE = 2EI/L2

    PcPc

  • 14

    2007-8-22 27

    Columns in a Mixed Frame (E.5)

    srV suV

    Effective length to be increase by f

    Storey buckling amplification factor

    = total vertical load in that storey in the columns that resist sway in that plane

    = total vertical load in that storey in the columns not resisting sway in that plane

    Rigid frame Simple frame

    2007-8-22 28

    Frames with partial sway bracing Two other plots exist as E4 & E5 Relate to kp =1 and kp =2

    For frames which do not satisfy the requirements for a non-sway frame, can still take advantage of the stiffness of the bracing using kp.

    kp is a measure of the stiffness of the partial sway bracing to the stiffness of the bare frame.

  • 15

    2007-8-22 29

    Frames with partial sway bracing(Annex E.3)

    kp = h2Sp/(80EKc) but 2

    c = sum of I/h for all the columns in that storey Sp = sum of the stiffness of every panel in the storey

    Sp = (0.6(h/b) ) t Ep/[1+(h/b)2]2

    h/b = ratio of storey height to panel width t = panel thickness Ep = modulus of elasticity of the panel material.

    To account for stiffening effect of infill wall panels in determining the effective length ratio for frame with partial wall bracing of relative stiffness kp

    Spring stiffness Sp

    h

    2007-8-22 30

    Kp = 1

    Kp =2

  • 16

    2007-8-22 31

    Amplified Sway Method

    Sway moment should be multiplied by the amplification factor kamp

    Non-sway mode in-plane effective length should be used.

    2007-8-22 32

    kamp for sway sensitive frames

    1) for unclad frames or for clad structures in which the stiffening effect of masonry infill wall panels or diaphragms of profiled steel sheeting is explicitly taken into account in determining cr :

    kamp = cr / (cr 1)

  • 17

    2007-8-22 33

    kamp for sway sensitive frames2) for clad structures,

    provided that the stiffening effect of masonry infill wall panels or diaphragms of profiled steel sheeting is not explicitly taken into account:kamp = cr / (1.15 cr 1.5) but 1.0

    Gives smaller amplification factors than previous slide.

    2007-8-22 34

    Sway effects

    In the case of a symmetrical frame, with symmetrical vertical loads, the sway effects can correctly be taken as comprising the forces and moments in the frame due to the horizontal loads.

  • 18

    2007-8-22 35

    Sway Moments

    In every other case it is necessary to separate moments into sway and non-sway components by either:

    a) Deducting the non-sway effects.

    b) Direct calculation.

    2007-8-22 36

    a) Deducting the non-sway effects:

    1) Analyse the frame under the actual restraint conditions.

    2) Add horizontal restraints at each floor or roof level to prevent sway, then analyse the frame again.

    3) Obtain the sway effects by deducting the second set of forces and moments from the first set.

    In 1) moments are due to sway + non-sway distortions.In 2) moments are due to non-sway distortions.In 3) moments are thus only due to sway distortions.

    The forces and moments from step 3 are the sway effects which require magnifying by kamp.

    Sway Moments

  • 19

    2007-8-22 37

    Deducting the non-sway effects

    Step 1Step 2

    Sway moment = Moment in Step 1 Moment in Step 2

    Design moment = nonsway moment + kamp.x Sway moment(step 2)

    2007-8-22 38

    b) Direct calculation:

    1) Analyse the frame with horizontal restraints added at each floor or roof level to prevent sway.

    2) Reverse the directions of the horizontal reactions produced, at the added horizontal restraint locations.

    3) Apply them as loads to the otherwise unloaded frame under the actual restraint conditions.

    4) Adopt the forces and moments from the second analysis (step 3) as the sway effects which require magnifying by kamp.

    Sway Moments

  • 20

    2007-8-22 39

    Direct calculation

    Step 2: Sway MomentStep 1 Nonsway moment

    R3

    R2

    R1

    R3

    R2

    R1

    Design moment = nonsway moment + kamp.x Sway momentStep 1 Step 2

    2007-8-22 40

    Elastic design of sway sensitive frames

    If cr < 4.0 then The frame is sensitive to instability effects.

    The kamp approach is not suitable and a full second order elastic analysis should be used.

  • 21

    2007-8-22 41

    Example : Use of Annex E : Effective lengths in a continuous multi-storey frame

    3.6m

    3.6m

    3.6m

    3.6m

    7.2m 7.2m 7.2m 7.2m

    1

    2

    3

    Ix beams = 21500cm

    Ix columns = 6090cm

    4

    4

    16kN/m72kN/m

    Factored dead plus live load

    Beams are supporting concrete slab, Kb = 1.0 I/L

    2007-8-22 42

    Check if the frame is a sway frame

    The notional horizontal force = 0.5% factored (dead plus imposed load) =

    at roof level F1 = 0.5 (16 x 28.8)/100 = 2.3 kNat each floor F2 = 0.5 (72 x 28.8)/100 = 10.4 kN

    16kN/m72kN/m

    Factored dead plus live load

    Inter-storeyF1

    F2

    F2

    F2

    deflections9mm

    8mm

    6mm

    4mm

  • 22

    2007-8-22 43

    Sway or non-sway frame

    The deflection in the lower storey exceeds h/2000 = 3600/2000 = 1.8mm and the frame is a sway frame.

    Only the upper storey does not violate the non-sway limit.

    (*these deflection values have been guessed and are not the result of an analysis!)

    2007-8-22 44

    Using Appendix E

    Column 1 Beams KTL = KTR = KBL = KBR = I/L =21500/720 = 29.9Columns KU = KC = KL = I/L = 6090/360 = 16.9Restraint factorsTop k1 = (KC+KU) / (KC + KU +KTL+KTR) = 0.36Bottom k2 = (KC+KL) / (KC + KL +KTL+KTR) = 0.36

    The frame is a sway frame; use Figure E.2LE/L = 1.27 i.e. LE = 1.27 x 3.6 = 4.57m

    If bracing were provided and the frame became a non-sway frame, the effective length ratio from Figure E.1 of the code would be 0.625 i.e. LE = 0.625 x 3.6 = 2.25m

    3.6m

    3.6m

    3.6m

    3.6m

    7.2m 7.2m 7.2m 7.2m

    1

    2

    3

  • 23

    2007-8-22 45

    0

    0.1

    0.2

    0.3

    0.4

    0.5

    0.6

    0.7

    0.8

    0.9

    1

    0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

    Pinned

    k 1

    Fixed

    k 2 PinnedFixed

    2007-8-22 46

    Column 2Beams KTL = KBL = I/L =21500/720 = 29.9Columns KC = KL = I/L = 6090/360 = 16.9

    End Restraint factorsTop k1 = (KC) / (KC +KTL) = 0.36Bottom k2 = (KC+KL) / (KC + KL +KTL) = 0.53

    Therefore as the frame is a sway frame From Figure E.2

    LE/L = 1.4 i.e. LE = 1.4 x 3.6 = 5.04m

    3.6m

    3.6m

    3.6m

    3.6m

    7.2m 7.2m 7.2m 7.2m

    1

    2

    3

  • 24

    2007-8-22 47

    Column 3Beams KTL = KTR = I/L =21500/720 = 29.9

    Columns KU = KC = I/L = 6090/360 = 16.9Restraint factorsTop k1 = (KC+KU) / (KC + KU +KTL+KTR) = 0.36Bottom k2 = (KC) / (KC + 0.1 x KC ) = 0.91

    Therefore as the frame is a sway frame from Figure E.2LE/L = 2.0 i.e. LE = 2.0 x 3.6 = 7.20m

    The design would then proceed as normal using the effective lengths calculated above.

    3.6m

    3.6m

    3.6m

    3.6m

    7.2m 7.2m 7.2m 7.2m

    1

    2

    3

    Column based is pinned

    2007-8-22 48

    If the column bases were rigid base stiffness is taken as column stiffness : cl. 5.1.3.2

    Column 3Beams KTL = KTR = I/L =21500/720 = 29.9Columns KU = KC = I/L = 6090/360 = 16.9

    End restraint factorsTop k1 = (KC+KU) / (KC + KU +KTL+KTR) = 0.36Bottom k2 = (KC) / (KC + KC ) = 0.50

    From Figure E.2 LE/L = 1.35 i.e. LE = 1.35 x 3.6 = 4.86m

    The effective length is much reduced and the column will be smaller but the cost of providing moment resisting foundations may out-weight the cost of the savings in steelwork. The fixity would also be beneficial in controlling sway deformations.

    1

    2

    3

  • 25

    2007-8-22 49

    If all floor beams carrying load exceeding 90% of their moment capacity

    Column 1 Beams KTL = KTR = KBL = KBR = 0Columns KU = KC = KL = I/L = 6090/360 = 16.9Restraint factors

    Top k1 = (KC+KU) / (KC + KU + 0+ 0) = 1Bottom k2 = (KC+KL) / (KC + KL + 0+ 0) = 1

    From Figure E.2, the effective length ratio would be equal to infinity.

    1

    2

    3

    2007-8-22 50

    Using the amplified sway method.Alternatively consider the design of the original frame using the amplified sway method.The maximum value of the sway index is in the lower storey and is given by

    = (u-l)/h = 4/3600 = 1.1 x 10-3The elastic critical load factor cr is then given by :

    cr = 1/(200) = 4.55 > 4.0 (Note this suggests a very flexible frame)Amplification factor = cr /(cr-1) = 4.55/(4.55-1) = 1.28The design can proceed using effective length ratios of nonsway frame and all the moments due to horizontaldeformations multiplied by 1.28.

  • 26

    2007-8-22 51

    EXAMPLE 2

    Notional Horizontal Load = 0.5% floor gravity load applied in one direction at a time.The frame is a sway frame in both direction.Column designed will be governed by buckling about the minor axis.Hence, design the member for buckling about the minor axis

    NHLx

    x

    y

    100 kN

    150 kN

    100 kN

    100 kN100 kN

    NHLy

    150 kN150 kN

    150 kN

    NHLy NHLx

    All members UC 152 x 152 x 37 S 275 steel

    2007-8-22 52

    Example 2 : Continue

    Alternate designProvide bracing to prevent side sway in the x direction as shown.

    Design the column as nonsway in the x direction, but consider sway effect in the y direction.

    NHLyNHLy

    x

    y

    100 kN

    100 kN

    NHLx150 kN

    100 kN

    100 kN

    100 kN100 kN

  • 27

    2007-8-22 53

    100kN 100kN 1kN

    1kN

    1.5kN

    1.5kN

    Lateral Deflection at the storey level (cm)

    1.503

    1.305

    0.942

    0.412

    100 100

    150 150

    150 150

    A

    B 3.5m

    3.5m

    3.5m

    3.5m

    3.5m

    Frame Classification for sway or nonsway Limiting value for uncladded frame h/2000 = 350/2000 = 0.175cmsince interstorey sway deflections due to notional load at all storey level are greater than the limiting value of 0.175cm, the frame is classified as sway frame.

    Example 2 : Continue. Consider sway effect in the y direction.

    Y direction

    NHL

    2007-8-22 54

    Compute Elastic Buckling Load FactorUse Annex E.6 and F.2Notional horizontal load in each storey = 0.5%(factored gravity loads).Conduct a linear elastic analysis to give sway deflection . F.2Compute sway indices for each storey s u Lstorey height=

    (Storey height = 350cm)

    0.0005640.0010430.0015120.001181

    Sway index, sStorey No.

    = 0.00151

    0.4311.300151.0200

    1200

    1

    maxscr

  • 28

    2007-8-22 55

    Column Effective Length

    Axial load in column AB, F = 504.7 kN

    Euler buckling load of column = 2EI/L2

    =

    Effective length factor for column AB

    48.17.504x311.3

    3667LEI

    LL

    2cr

    2E ==

    =

    A

    B

    504.7 kN

    504.7 kN

    2.7 kNm

    5.973 kNm

    Forces in column AB(from structural analysis

    Alternatively, we may use the limited frame method,Beam stiffness kb = 1.5I/L (Sway mode, Table E.1 in Annex E)kbottom = 0.5 (Nominal rigid base, Cl 5.1.3.2)

    5.05.1011

    11ktop =++++= 53.1

    LLE =

    Let us proceed with the calculation!

    2007-8-22 56

    For UC 152 x 152 x 37 S 275 steel, use design table Page 265Local Capacity Check (Simplified formula)

    Overall Buckling Check (simplified formula)

    (In-Plane Buckling )

    (Lateral Torsional Buckling)

    OK0.146.00703.039.085973.5

    13007.504

    MM

    AF

    cx

    x

    y

  • 29

    2007-8-22 57

    By Amplified Sway Method

    Af = =

    Column effective length for nonsway framekbottom = 0.5 (Nominal rigid base, Cl 5.1.3.2)Beam stiffness = 0.5I/L (Non-sway mode, Table E.1 in Annex E)Ktop = (1 + 1)/(1+ 1 + 0.5) = 0.8In-plane Column effective length factor = 0.77 (Fig. E.1, Annex E for nonsway frame)Lex=3.5m x 0.77 =2.7m Pcx = 1180kN In planeLey = 3.5m Pcy = 668kN out-of-plane = -2.7/5.973 = - 0.452 mLT = 0.45 (Table 18 of BS5950)mx = 0.51 (Table 26 of BS5950)In Plane Buckling

    Lateral Torsional Buckling (out of plane buckling; no amplification for moment)

    OK

    1crcr

    43.1

    131.331.3 =

    0.180.075

    97.5x51.0x43.1668

    7.504Z

    MmkPF

    yy

    xxamp

    c

    4 cycles/second(including interaction between primary and secondary beams)

    Building deflection (< H/500) Stability, Overturning & Uplift (foundation and continuity of column) Building frequencies (Period < 2 seconds) Continuity of floor diaphragms Continuity of vertical bracing Location of lateral bracing

  • 30

    2007-8-22 59

    Disproportionate Collapse

    2007-8-22 60

    Structural Integrity

    Deflected shapeR

    1 Tying force = R or 75 kN

  • 31

    2007-8-22 61

    Avoidance of Disproportionate Collapse2 Tying of columns

    2007-8-22 62

    3.Continuity of columns. all columns should be carried through at each beam-to-column connection. All column splices should be capable of resisting a tensile force equal to the largest factored vertical dead and imposed load reaction applied to the column at a single floor level

    4.Resistance to horizontal forces. Braced bays or other systems for resisting horizontal forces should be distributed throughout the building such that, in each of two directions approximately at right angles.

    5.Heavy floor units. Where precast concrete or other heavy floor or roof units are used they should be effectively anchored in the direction of their span

  • 32

    2007-8-22 63

    If the five criteria are not satisfied

    Check disproportionate collapse: to ensure that removal of single element does not cause too large an area (15% of floor area or 70m2) to collapse

    If large area collapse occurs, design the key element to withstand a blast of 34 kN/m2

    2007-8-22 64

    Check disproportionate collapse: to ensure that removal of single element does not cause too large an area (15% of floor area or 70m2) to collapse

    If large area collapse occurs, design the key element to withstand the blast pressure

    Alternate Load Path Method

    Core

    Exterior columns

    Belt and outrigger

  • 33

    2007-8-22 65

    Progressive Collapse Resistant Design

    Local Resistance Method:

    This method seeks to provide sufficient strength to resist an extreme loading event. It requires that a specific collapse-initiating event be identified so that the local resistance can be referenced to a specific limit state.

    Alternate Load Path Method

    This method requires that the structure is able to provide alternate load path to one lost column. The collapse-initiating event and threat level is not considered.

    2007-8-22 66

    Design SummaryElastic Design

    Classify frames as braced or unbraced frame (5.1.4), and sway or nonsway (2.4.2.6).

    Independently braced frames (5.6.2): Design to resist gravity loads (load combination 1). The non-sway mode effective length of the columns should be

    found from Annex E. Pattern loading should be used to determine the most severe

    moments and forces. Sub-frames may be used to reduce the number of load cases. The stabilizing system must be designed to resist all the horizontal

    loads applied including the notional horizontal forces.

  • 34

    2007-8-22 67

    Elastic Non-sway frames (5.6.3):

    Design to resist gravity loads (load combination 1) The non-sway mode effective length of the columns

    should be found from Annex E. Pattern loading should be used to determine the most

    severe moments and forces. Sub-frames may be used to reduce the number of

    load cases. The frame should be checked for combined vertical

    and horizontal loads without pattern loading.

    Design SummaryElastic Design

    2007-8-22 68

    Elastic sway sensitive frames Check in the non-sway mode i.e. design to resist

    gravity loads (load combination1) as for independently braced frames without taking account of sway. (without notional horizontal forces, but with pattern loading).

    Check in the sway mode for gravity load (i.e. load combination 1) plus the notional horizontal forces without any pattern loading.

    Check in the sway mode for combined vertical and horizontal loads (i.e. load combinations 2 and 3) without pattern loading.

    Allow for sway using the effective length methodAnnex E or the amplified sway method.

    Design SummaryElastic Design

  • 35

    2007-8-22 69

    Reading assignment:

    BS5950:Part1 Cls 5.1, 5.2 & 5.6

    R Liew note: Chapter 3 Sections 3

    HOMEWORK 4: CONTINUOUS FRAMES

    2007-8-22 70

    Take Home Design Project

    DL =24kN/mIL= 30 kN/m

    6m

    Storey height =4m

    6m 6m 6m

    Five framesSpacing 6m

    Comment on the structural integrity

  • 36

    2007-8-22 71

    PLASTIC DESIGN

    2007-8-22 72

    Plastic design

    Classify frames as independently braced (5.7.2), sway or non sway (5.7.3)

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    2007-8-22 73

    Plastic braced frames

    Independently braced frames (5.7.2) Design to resist gravity loads (load

    combination 1). The effective length LE of the columns in the

    plane of the frame should generally be taken as equal to the storey height L.

    Check columns under pattern loading using an effective length from Annex E.

    2007-8-22 74

    Plastic design of non-sway frames

    If beams are designed plastically,they will contain moments in excess of 90% of Mp.Care must be taken when using Annex Eremembering that Kb is likely to be ZERO in most cases,giving LE/L factors close to 1.0

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    2007-8-22 75

    Plastic design of non-sway frames

    Normal plastic rules apply for local capacityand member stability as for portal frames. Usually the latter will be less onerous due to the presence of floor slabs to provide stability to the beams.

    Remember that the frame must be stable in the plane perpendicular to the plane of the frame being designed.

    2007-8-22 76

    Plastic design- unbraced frames

    Check for possible non-sway modes of failure as recommended for independently braced frames.

    Satisfy the simplified M-R-Wood frame stability check (given in clause 5.7.3.2),

    Or design to resist sway mode failure using either elastic analysis or second order elastic-plastic analysis.

  • 39

    2007-8-22 77

    Plastic design of sway frames

    Frames may be designed using a second order elastic-plastic analysis or by using the sway stability check.

    This is derived from the Merchant-Rankine-Wood equation.

    Origins: The Rankine strut equation is1/PF = 1/PCR + 1/ PSQ

    2007-8-22 78

    M-R-Wood equation

    Rankines formula proposed for struts prior to development of Ayrton-Perry equation.

    Merchant suggested its use for frames with: Elastic critical load replacing Euler load. Plastic collapse load replacing squash load.

  • 40

    2007-8-22 79

    Plastic design of sway framesMerchant-Rankine Equation

    1 = 1 + 1PF Psq

    Pcr

    Psq/Pcr

    PF/Psq

    Merchant-Rankine1.0

    1.0

    0.5

    2007-8-22 80

    Development of M-R-Wood Eqn 1/PF = 1/PCR + 1/ PSQ

    1/F = 1/ CR + 1/ P ={ P + CR }/CR P

    F = CR P / { P + CR } But F = 1 P + CR = CR P CR = CR P - P = P {CR 1} P = CR /{CR 1}

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    2007-8-22 81

    Development of M-R-Wood Eqn

    But for CR/ P >10stray composite action &strain hardening means noneed to reduce r below P.

    For 10 < CR/ P < 4.0change 1 to 0.9 for continuity at CR/ P =10

    r = 0.9CR /{CR 1}

    r P

    P /CR0.1 0.25

    Merchant Rankine-Wood

    Merchant-Rankine

    2007-8-22 82

    Combined plastic collapse mechanism

    Determine plastic collapse load using sway mode shown

  • 42

    2007-8-22 83

    Plastic collapse load

    1. The bases of the columns should be fixed.2. Mechanism as on previous slide.3. Ensure that columns remain elastic at

    assumed plastic moment.4. Check that no localised beam or storey

    mechanism is more dangerous.5. Storey height less than mean column

    spacing.

    2007-8-22 84

    Development of M-R-Wood EqnFor actual unclad frames or clad frames

    where cladding stiffness is utilised

    For CR / P > 20strain hardening means noneed to reduce r below P . For 20 < CR/ P < 5.75change 1 to 0.95 for continuity at CR/ P = 20

    r = 0.95CR /{CR 1}

    r P

    P /CR0.1 0.25

    0.05