Model ID: 1371
Flow Duct
Results are presented for situations with as well as without a compressible irrotational background flow and for the cases of hard and lined duct walls.
|
AEROSPACE: The modeling of aircraft-engine noise is a central problem in the field of computational aeroacoustics. This result shows the logarithmic pressure field in a jet engine. |
Application Areas
Products Used
Similar Models
- Piezo-Acoustic Transducer
- Jet Pipe
- Acoustic-Structure Interaction
- Loudspeaker Driver
- Ultrasound Scattering Off a Cylinder

