04 section3 mass modelling input 012904

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  • 7/28/2019 04 Section3 Mass Modelling Input 012904

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    NAS122, Section 3, January 2004

    Copyright 2004 MSC.Software Corporation

    SECTION 3

    MASS MODELING

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    NAS122, Section 3, January 2004

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    TABLE OF CONTENTS

    Page

    MASS MODELING 3-4

    COUPLED VERSUS LUMPED MASS 3-5

    ROD FINITE ELEMENT EXAMPLE 3-7

    JUSTIFICATION FOR MSC.NASTRAN COUPLED MASS CONVENTION 3-9

    MASS UNITS 3-11

    MASS INPUT 3-12

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    MASS MODELING

    This section considers some of the implications of Mass Modeling This section describes the Coupled versus Lumped mass representations

    previously mentioned.

    Review the units of Mass

    Also show how to set up different types of mass in Patran and theimplications in Nastran

    Density defined on a Material Property entry

    Non-Structural mass defined on element Physical Property entry

    Mass elements defined as CONM1, CONM2 or CMASS1

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    COUPLED VERSUS LUMPED MASS

    Coupled mass is generally more accurate than lumped mass (however itreally needs both methods to be assessed in each case)

    Lumped mass is preferred for computational speed in dynamic analysis.

    User-selectable coupled mass matrix for elements

    PARAM, COUPMASS, 1 to select coupled mass

    The default is lumped mass.

    Elements which have either lumped or coupled mass:

    BAR, BEAM, CONROD, HEXA, PENTA, QUAD4, QUAD8, ROD, TETRA,

    TRIA3, TRIA6, TRIAX6, TUBE

    Elements which have lumped mass only: CONEAX, SHEAR

    Elements which have coupled mass only:

    BEND, HEX20, TRAPRG, TRIARG

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    COUPLED VERSUS LUMPED MASS (Cont.) Lumped mass contains only diagonal, translational

    components (no rotational ones).

    Coupled mass contains off-diagonal translational components

    as well as rotations for BAR (though no torsion), BEAM, and

    BEND elements.

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    ROD FINITE ELEMENT EXAMPLE

    Stiffness matrix:

    Classical consistent mass:

    Length = L, Area = A, Torsional Constant = J, Youngs

    Modulus = E, Shear modulus = G

    AE

    L

    -AE

    L0 0

    GJ

    L

    -GJ

    L0

    -AEL

    AE

    L0 0

    0

    -GJ

    L00

    GJ

    L

    k =

    21

    43

    L

    0 0

    I3A

    0

    0 0

    0m = AL

    I6A

    I6A

    00I3A

    1/3

    1/6 1/3

    1/6

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    ROD FINITE ELEMENT EXAMPLE(Cont.) Classical and MSC.NASTRAN lumped mass:

    MSC.NASTRAN coupled mass:

    The translational terms represent the average of lumped mass and classical consistent mass. Thisaverage is found to be best for ROD and BAR elements.

    0 0

    0

    0 0

    0m = AL

    00

    1/2

    0 1/2

    0

    0 0

    00

    0 0

    0

    0 0

    0m = AL

    00

    5/12

    1/12 5/12

    1/12

    0 0

    0 0

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    NAS122, Section 3, January 2004

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    JUSTIFICATION FOR MSC.NASTRANCOUPLED MASS CONVENTION

    Consider a fixed-free rod

    Exact quarter-wave natural frequency

    u(t)

    Single Element

    2

    1

    L

    1/4 = = 1.5708 E/

    2 L

    E/

    L

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    JUSTIFICATION FOR MSC.NASTRANCOUPLED MASSS CONVENTION (Cont.)

    Different approximations Lumped mass

    Classical consistent mass

    MSC.NASTRAN Coupled mass

    L = = 1.414E/

    L

    E/

    L2

    (-10%)

    L = = 1.732E/

    L

    E/ L

    3(+10%)

    L = = 1.549E/

    L

    E/ L

    12/5(-1.4%)

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    MASS UNITS MSC.NASTRAN assumes consistent units. YOU MUST BE CAREFUL.

    Weight units may be input instead of mass units if this is more convenient. You

    must then convert them to mass units using PARAM,WTMASS.

    Weight-to-mass conversion:

    Mass = (1/G) Weight (G = Gravity Acceleration)

    Mass Density = (1/G) Weight Density

    PARAM,WTMASS, factor performs conversion with factor = 1/G. The default

    value for factor is 1.0.

    Example:

    Input RHO = 0.3 lb/in3 for steel weight density.

    Use PARAM,WTMASS,0.00259 for G = 386.4 in/sec2.

    PARAM,WTMASS is used once per run and multiplies all weight/mass input

    (including MASSi, CONMi, and nonstructural mass input). Do not mix input

    types. Use all mass or all weight inputs.

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    MASS INPUT The most common way to define Mass in a structure is via the material density of

    each of the materials in the structure. This is done using the Material Propertiesform. Every element that references the material property will build an element

    mass matrix.

    MATi entries

    1 2 3 4 5 6 7 8 9 10

    MAT1 MID E G NU RHO A TREF GE

    MAT1 2 30.0E6 0.3 7.7E-4

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    MASS INPUT (Cont.) Nonstructural mass

    Mass input on element property entry which is not associated with geometric

    properties of element. Input as mass/length for line elements and mass/area forelements with 2-D geometry.

    Examples are: payload distributed over a floor, insulation on beams, mass of electroniccomponent modeled on a PCB.

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    MASS INPUT (Cont.) Scalar mass

    The Type of Grid Point Mass available are CONM1 and CONM2. CONM2 ismost common. The selection between them is made using the Option:

    COUPLED gives a CONM1 (A full 6x6 mass matrix) - The user defines half of

    the terms, symmetry is assumed. This is only used for advanced mass

    definitions and is not very commonly seen

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    MASS INPUT (Cont.)

    Lumped gives a CONM2 (concentrated mass), where the translationaland rotational terms are defined

    333231

    2221

    11

    III

    II

    I

    M

    SYMM

    M

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    MASS INPUT (Cont.)

    Grounded gives a CMASS1 (scalar mass) This entry permits a mass with a value in a single direction, this can be a useful

    modeling technique when mass is only considered effective in that direction

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    MASS INPUT (Cont.)

    The most common form of Scalar element Mass input is via aCONM2

    If only a mass term M is required then the other terms are left blank

    and the mass will have translational mass terms, equal in the 3

    directions

    If inertia properties are required, then these are entered as

    appropriate

    If the mass cg is offset from the grid position, then this is also

    defined (this writes an MPC equation into the mass matrixeffectively a rigid offset)

    CONM2s are frequently defined with an offset and linked to more

    than one grid point with an RBE2 or RBE3, depending on the

    nature of the structure being attached to