Harmonic Balance equations describe periodic unsteady flows where the unsteady frequencies are known beforehand. They are suited to modeling periodically repeating flow fields that typically occur in turbomachinery such as compressors, turbines, and fans.
The Harmonic Balance method in
Simcenter STAR-CCM+ is a full decomposition of the Navier-Stokes equations in the frequency domain. The unsteady, transient flow is represented in the frequency domain as a Fourier series in time. All transport equations for momentum, energy, and turbulence are decomposed into the frequency domain on the basis of fundamental driving modes, usually a blade-passing frequency or repeating wake modes. Steady-state equations representing the unsteady solution at discrete time levels in a single unsteady period are solved to obtain the Fourier coefficients.
The number of time levels required depends on the number of modes retained in the problem. The steady-state solution in every time level is implicitly coupled at the periodic boundaries by the physical time derivatives. The linear system is then subjected to approximate factorization to achieve implicit coupling between time levels.
Governing Equations
The governing equations for harmonic balance are the Navier-Stokes equations in integral form for a rigid, arbitrary control volume with differential surface area in a relative frame of reference rotating steadily with angular velocity .
Figure 1. EQUATION_DISPLAY
(5042)
where:
is the solution vector of conservation variables, .
is the inviscid flux, .
is the viscous flux, .
is the source vector, .
and:
is the density.
is the absolute velocity.
is the relative velocity, .
is the total enthalpy.
is the pressure.
is the shear stress tensor.
is the heat flux.
is a user-defined source term.
Harmonic Balance Equations
Since the solution to the governing equations is periodic in time, it can be represented by a Fourier series:
Figure 2. EQUATION_DISPLAY
(5043)
where:
is the fundamental frequency of the disturbance.
is the number of harmonics retained in the solution.
are the Fourier coefficients, uniquely determined from the discrete Fourier transform:
Figure 3. EQUATION_DISPLAY
(5044)
where are a set of solutions at discrete time levels distributed throughout one period of unsteadiness .
At any location in the flowfield domain, the time-level solutions can be transformed into Fourier coefficients and
vice versa using a discrete Fourier transform operator and its corresponding inverse as follows:
Figure 4. EQUATION_DISPLAY
(5045)
Figure 5. EQUATION_DISPLAY
(5046)
where and are square matrices of dimension and the Fourier coefficients and time-level solutions have been assembled into the vectors and :
The solutions at each discrete time level are obtained by applying the governing equations
Eqn. (5042) to all the simultaneously:
Figure 6. EQUATION_DISPLAY
(5047)
where the flux and source vectors , , and are evaluated using the corresponding time-level solution. Example:
The time derivative in
Eqn. (5047) is evaluated by differentiating
Eqn. (5047) with respect to time, then using
Eqn. (5045) as follows:
or
Figure 7. EQUATION_DISPLAY
(5048)
where is the pseudo-spectral operator. Substituting
Eqn. (5048) for the time derivative in
Eqn. (5047) yields the final harmonic balance equation: