Structural Design Theories

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    Statically Determinate Beams

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    SF & BM Diagrams - Single Concentrated Load

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    SF & BM Diagrams - Uniformly Distributed Load

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    Calculation of the Second Moment of Area I

    Item Area =A y A.y h A.h A.h2 INA

    1 44 x 6 264 97 25608 36.87 9734 358880 790

    2 25 x 6 150 87.5 13125 27.37 4106 112370 7810

    3 47 x 3 141 1.5 212 58.63 8267 484680 100

    4 25 x 3 75 12.5 938 47.63 3572 170150 3900

    5 86 x 2 172 48.5 8342 11.63 2000 23260 106000

    SUM 802 48225 1149340 118600

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    Effective Bending Section - Buckled Web

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    Stresses Due to Bending Moment

    Figure 5/6a

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    Stresses Due to Bending Plus End Load

    Figure 5/6b

    Eff i D h f B

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    Effective Depth of Beam

    BM = 8 KNm

    Couple P = 8/91 = 87.9 KN

    Area of Compression Flange = 44 x 6 + 16 x 8 = 392 mm2

    Area of Tension Flange = 47 x 3 + 16 x 5 = 221 mm2

    I iti l E ti t f L d i St i

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    Initial Estimate of Loads in Stringers

    D fl ti f C til ith

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    Deflection of Cantilever withConcentrated Load at Tip

    Deflection of Simply Supported Beam

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    Deflection of Simply Supported Beamwith Uniformly Distributed Load

    Example Beam Deflection

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    Example - Beam Deflection

    Calculate the maximum deflection at the centre-line

    and weight of the top and bottom skins

    E = 110000 N/mm2 (Titanium)

    Allowable stress - Top = 675 N/mm2

    B 750 N/ 2

    Tornado Carry through Box

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    Tornado Carry-through Box

    Plastic Bending

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    Plastic Bending

    Allowable Moment - Plastic & Elastic Bending

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    Allowable Moment - Plastic & Elastic Bending

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    Plastic Bending - Assumed Stress Distribution

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    Plastic Bending Assumed Stress Distribution

    Statically Determinate &

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    Statically Determinate &Statically Indeterminate Structures

    Strain Energy in Tension

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    St a e gy e s o

    Example 1 - Strain Energy - Propped Cantilever

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    p gy pp

    Example 2 - Strain Energy - Beam on 3 Supports

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    p gy pp

    Deflection of a Cantilever Beam

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    Deflection of a Simply Supported Beam

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    Determine maximum deflection at centre of beam

    E = 72000 N/mm2 I = 1.2 x 106 mm4

    Using Castiglianos Theorem

    Apply load P at centre of beam

    Theorem of Three Moments

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    Example of Theorem of Three Moments

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    Example - Theorem of Three Moments

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    For the above beam, draw the BM and SF diagrams

    Use the theorem of three moments

    Assume EI are constant

    FIGURE5/24

    Shear Stress Distribution - Rectangular Section

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    Shear Stress Distribution - I beams

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    Shear Stress Distribution inFl f Ch l & I S ti

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    Flanges of Channel & I Section

    Complementary Shear Stress

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    Web Shear Flows

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    Example Shear Flows & End Loads

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    FIGURE5/30

    Calculate the shear flow in the web and the load distribution in the members