A linearized theory for swirling supersonic jets and its application to shock-cell noise
Abstract
- Publication:
-
AIAA Journal
- Pub Date:
- December 1985
- DOI:
- 10.2514/3.9194
- Bibcode:
- 1985AIAAJ..23.1902C
- Keywords:
-
- Jet Aircraft Noise;
- Linearization;
- Noise Generators;
- Shock Wave Interaction;
- Supersonic Jet Flow;
- Swirling;
- Inviscid Flow;
- Method Of Characteristics;
- Nozzle Flow;
- Shock Wave Profiles;
- Supersonic Nozzles;
- Fluid Mechanics and Heat Transfer