For an HBM cyclic analysis, the dynamics equations of a cyclically symmetric structure are transformed to cyclic coordinates (see The General Cyclic Symmetry Analysis Equations) leading to decoupled system matrices.
The structure is subjected to a traveling wave excitation whose fundamental harmonic
has engine order (EO), , which is referred to as the fundamental engine order, with higher
time harmonics,
, having the engine order
. This excitation may be represented as [9]:
(1–19) |
where the force applied on the sector is given by [9]:
(1–20) |
where:
(1–21) |
Substituting Equation 1–20 into Equation 1–19 we obtain:
(1–22) |
where:
(1–23) |
where:
Note that is equal to some scalar multiple of a column of the complex Fourier
matrix. Thus,
is the unique spatial harmonic associated with the time harmonic,
, of the traveling wave excitation, whose fundamental harmonic has
engine order
.
In HBM analysis, the displacement solution and the internal forces are assumed to be harmonic with:
(1–24) |
(1–25) |
Substituting into Equation 1–5 and
equating coefficients of , the equation of motion in the frequency domain in physical
coordinates for time harmonic,
, is obtained:
(1–26) |
Because the time harmonic, , is associated with only the spatial harmonic,
, it is isolated by pre-multiplying the equation above by
:
(1–27) |
Due to the block-circulant structure of the matrices of a cyclic symmetric structure [10] and the properties of columns of a Fourier matrix, the nonzero rows of the above equation reduce to:
(1–28) |
which is the equation of motion in cyclic coordinates.
(1–29) |
(1–30) |
where:
Subscripts |
(1–31) |
Note that the direction of the traveling wave component for harmonic, , in the equation above (for
and
) is reversed from the direction of the fundamental EO if
.
may be further reduced by using reduction techniques such as component
mode synthesis.