Fong743 DEX Plots 1 to 11 Isotropic Canti Beam

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    x x

    x x

    x x

    x

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    Ordered Data Plot

    Settings

    ResponseY(FirstResonanceFreq)

    + + + + - - -X1: - - + + - - +X2:- + - + - + -X3:

    Free Vibration of an Isotropic Cantilever Beam using FEM Abaqu

    k = 3n = 8

    Step 1

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    170

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    Main Effects Plot

    Factors

    MeanResponseY

    (FirstResonanceFreq)

    X1

    L

    X2

    t

    X3

    E

    - + - + - +

    -11.6148

    -6.%

    9.28075

    5%

    0.18075

    0%

    Free Vibration of an Isotropic Cantilever Beam using FEM Abaqus

    k = 3n = 8

    Step 3

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    170

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    X1(L)

    AverageY(First

    ResonanceFreq) 1: -11.61 12: -0.3 13: -0.01

    X2(t)

    2: 9.28 23: 0

    X3(E)

    3: 0.18

    Free Vibration of an Isotropic Cantilever Beam using FEM Abaqus

    Interaction Effects Matrix

    Step 4

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    - -

    - -

    + +

    + +

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    Factor Combinations

    AverageY(FirstReson

    anceFreq) x1(L)

    - -

    - -

    + +

    + +

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    Factor Combinations

    AverageY(FirstReson

    anceFreq) x2(t)

    -

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    -+

    +

    +

    +

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    Factor Combinations

    AverageY(FirstResonanceFreq) x3(E)

    Free Vibration of an Isotropic Cantilever Beam using FEM Abaqus

    Block Plots

    Step 5

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    170 175 180 185

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    Youden Plot

    Response Y (First Resonance Freq) for - Setting

    ResponseY(FirstRes

    onanceFreq)for+

    Setting

    1

    2

    1231323123

    Free Vibration of an Isotropic Cantilever Beam using FEM Abaqus

    k = 3n = 8

    Step 6

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    0

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    |Effects| Plot

    Factor

    |E

    ffects|

    Free Vibration of an Isotropic Cantilever Beam using FEM Abaqus

    1 2 12 3 13 23

    Factor Effect

    1 : -112 : 9.212 : -0.

    3 : 0.113 : -0.23 : 0.0123 : 0.0

    Average = 181.1914

    Step 7

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    x x x x x

    x

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    Halfnormal Probability Plot of |Effects|

    Halfnormal Distribution Order Statistic Medians

    Order

    ed|Effects|

    Free Vibration of an Isotropic Cantilever Beam using FEM Abaqus

    k = 3n = 8

    Step 8

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    Cumulative Residual SD Plot

    Cumulative Model

    Res

    idualSD

    1 2 12 3 13 23Average

    Free Vibration of an Isotropic Cantilever Beam using FEM Abaqus

    k = 3n = 8

    Step 9

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    -2 -1 0 1

    -2

    -1

    0

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    Contour Plot of the 2 Dominant Factors: X1 (L) and X2 (t)

    X1(L)

    X2(t)

    -2 -1 0 1

    -2

    -1

    0

    1

    2

    -2 -1 0 1

    -2

    -1

    0

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    -2 -1 0 1

    -2

    -1

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    -2 -1 0 1

    -2

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    -2 -1 0 1

    -2

    -1

    0

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    -2 -1 0 1

    -2

    -1

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    -2 -1 0 1

    -2

    -1

    0

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    -2 -1 0 1

    -2

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    -2 -1 0 1

    -2

    -1

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    -2 -1 0 1

    -2

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    -2 -1 0 1

    -2

    -1

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    -2 -1 0 1

    -2

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    -2 -1 0 1

    -2

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    -2 -1 0 1

    -2

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    -2 -1 0 1

    -2

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    -2 -1 0 1

    -2

    -1

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    182.21 170.892

    191.7875 179.876

    Free Vibration of an Isotropic Cantilever Beam using FEM AbaqusStep 10

    Model Predicted Value at Center Point = 181.1914

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    146 164.25 182.5 200.75

    0

    0.05

    0.1

    0.15

    0.2

    Resonance Freq. Q1 ( kHz ) (n = 9, s = 3.

    Prob

    ability

    Free Bending Vibration of an Isotropic Cantilever Beam ( FE

    95% Uncertainty Bounds Plot with Dataplot (Fong-Marcal-Filli

    "DEX" = Design of

    Experiments, where

    k = no. of factors,

    n = no. of runs.

    Resonance Freq.

    181.1(for a 9 - run "D

    n = 8 plus

    95% Lower

    Bound =

    171.514

    95%

    Bo

    190

    L = 0.232 mm +/- 1.6 %, h = 0.007 mm +/- 2.5 %, E = 169,158 MPa +

    *Timoshenko-Young, Vibration Problems in Eng., 3rd ed

    Exact solution*: Qt-statistic = (181.18 - 179

    = 2.154 / ( 3.72Critical t ( 0.025, 8) = 2.30

    Conclusion: FEM simula

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