Aeroacoustics Interfaces
T
his chapter describes the physics interfaces found under the
Aeroacoustics
branch
.
The aeroacoustic branch has physics interfaces to solve the fully linearized acoustic equation for several physical conditions, they are: the
linearized Euler
(LE) equations, the
linearized Navier-Stokes
(LNS) equations, and the
linearized potential flow
(LPF)
equations.
In this chapter:
•
The Linearized Euler, Frequency Domain Interface
•
The Linearized Euler, Transient Interface
•
The Linearized Navier-Stokes, Frequency Domain Interface
•
The Linearized Navier-Stokes, Transient Interface
•
The Linearized Potential Flow, Frequency Domain Interface
•
The Linearized Potential Flow, Transient Interface
•
The Linearized Potential Flow, Boundary Mode Interface
•
The Compressible Potential Flow Interface
•
Modeling with the Aeroacoustics Branch
•
Theory Background for the Aeroacoustics Branch
•
References for the Aeroacoustics Branch Interfaces
