带声衬的通用发动机短舱
Application ID: 141081
This model demonstrates two approaches to model the acoustics in a generic nacelle with an acoustic liner and a background flow. The first method uses the Compressible Potential Flow and the* Linearized Potential Flow, Frequency Domain* interfaces, while the second, more detailed approach, uses a turbulent background flow and the Linearized Navier–Stokes, Frequency Domain interface.
In the first approach, based on a linearized potential flow equations, the acoustic liner is modeled using the Brambley option for the impedance condition. This is an extended version of the Ingard–Myers boundary condition which takes into account the thickness of the turbulent boundary layer of the background flow field. A propagating acoustic mode with a radial and azimuthal wave number is actuated using a Port condition.
In the second approach, based on the linearized Navier–Stokes equations, the propagating modes are found with the Linearized Navier–Stokes, Boundary Mode interface and then used as a background field to excite the system with the correct acoustic mode. The results of the two approaches are compared.
案例中展示的此类问题通常可通过以下产品建模:
您可能需要以下相关模块才能创建并运行这个模型,包括:
- COMSOL Multiphysics® 和
- 声学模块 和
- 以下模块之一: CFD 模块, 或 传热模块
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