Basic Random

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    Basic Random Analysis

    First, the frequency response analysis is performed for sinusoidal loading conditions, {Pa}, each a

    separate subcase, at a sequence of frequencies i. The results are output to a normal XDB results

    file.

    Subcases in Dynamic Analysis

    Some of the statics options that are not available in dynamic response analysis and complex

    eigenvalue analysis include:

    Changes in boundary conditions between subcases

    Grid point forces and element strain energy outputs

    4.Multiple subcases are available for frequency response analysis (SOLs 108,111and 118) for the

    purpose of solving multiple loading conditions more efficiently.(Each frequency requires a matrix

    decomposition and each additional load vector may be processed at this time with small cost.)

    Another use is in random analysis where several loads need to be combined, each with a

    different spectral density distribution

    Recommendations

    The following guidelines should be observed when applying dynamic loads:

    TABLEDi

    1.Tables are extrapolated at each end from the first or last two points. If the load actually

    goes to zero, add two points with values of y = 0.

    2.Linear interpolation is used between tabular points.

    3.If a jump occurs (two points with equal values of X), the value of Y at the jump is the

    average of the two points.

    Stress analysis should be performed at the detailed part level with the loads from the model. The

    use of element stresses directly from the output of the model requires detailed review in most

    cases.

    Effective thicknesses or reduced bending properties may have been used to reflect panel cutouts

    or partial beam and fixity.

    This piece-part assessment ensures a check and balance of the finite element model and the stress

    distributions visualized and treated by the element selection. Also, the source of the components

    of stress are known, that is, whether the predominant stress component is due to bending or axial

    loads.

    One area in which an underestimation of load could occur is the local response of small masses

    during a dynamic analysis. These should be addressed in the detailed stress analysis with both the

    model predictions and an alternate loading such as a specified loading condition. For the model to

    give correct loads for the local response of a mass, one needs all of the following:

    Mass must be represented by enough points to characterize the energy of the critical

    local mode (a single-point mass may not be sufficient).

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    Mass must be supported by proper elastic elements to represent the local mode(RBE2 or

    RBE3 may not be sufficient).

    Mass must be in the ASET.

    Model and all analysis (input spectra, etc.) must be carried beyond this local critical

    mode (as far as frequency is concerned).

    Setup for Random Analysis

    An Nastran random analysis requires a preliminary frequency response analysis to generate the

    proper transfer functions that define the output/input ratios. The squared magnitudes of the

    results are then multiplied by the spectral density functions of the actual loads. Normally, theinputs are unit loads (e.g., one g constant magnitude base excitation or a unit pressure on a

    surface).

    VM Stress

    Since these values are Root-Mean-Square (RMS) they will always be positive. This means that

    combining these values to obtain a maximum resultant is not purely valid. Many FEA codes will

    calculate maximum displacement, Von Mises stress or Principal stresses based on Random

    Vibration results.

    It is important to remember that these calculations are based on all positive component values

    and will not be accurate.

    Loads may be input as base accelerations or applied external loads. The base excitation option

    assumes that the input load will excite any part of the structure that has a constraint or is attached

    by a spring to ground. The excitation is always defined as a linear acceleration.

    RMS measures in Random Vibration problems, because all frequencies are acting simultaneously

    and the RMS values represent the square root of the area under the PSD curve. Statistically it

    represents the 1-sigma results.

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    For Dynamic Frequency and Random analysis studies damping will have a big impact on the

    maximum response. Zero damping should not be used since the response will try to be infinite. For

    Random studies damping will have less of an impact on RMS results since the RMS values equal

    the square root of the area under the PSD response curves.

    The critical components and their potential high stress areas (hot spots) are determined from the

    strain energy density (SED) information of the normal mode analysis.

    Von Mises Stress in Random Analysis

    The RMS of basic stress tensor can not be used to calculate von Mises stresses. The probability

    distribution of von Mises stress is not Gaussian, nor is it centered about zero as basic stress tensor

    is.

    EQUIVALENT VON MISES STRESS

    When the excitation is random, the principal directions can rotate continuously with time ;

    the von Mises stress is proportional to the root mean

    square of the shear stress over all planes.

    The first method is based on the definition

    of the von Mises stress as a uniaxial random process for which the PSD function is computed. The

    second one is a frequency domain formulation of the

    multiaxial rainflow method. Both methods lead to

    a similar implementation and damage maps, to localize the most critical elements.