Howling in a Model-Scale Nozzle Related to Shock-Induced Boundary-Layer Separation at the Nozzle Exit
Author:
Affiliation:
1. Georgia Institute of Technology
2. Gulfstream Aerospace Corp
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3933
Reference32 articles.
1. Self-Excited Jet from a Low-Bypass Confluent Nozzle at Unity Extraction Ratio
2. Mixing of Exhaust and By-pass Flow in a By-pass Engine
3. Practical Bypass Mixing Systems for Fan Jet Aero Engines
4. Noise reduction with lobed mixers - Nozzle-length and free-jet speed effects
5. Noise of Internally Mixed Exhaust Systems With External Plug For Supersonic Transport Applications
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1. Low-Order Empirical Noise Modeling of Internally Mixed Exhaust Systems;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
2. Computational Aeroacoustic Study of Coannular Nozzles with Internal Mixing Geometries at High Transonic Mach Numbers;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
3. Howling in a Model-Scale Internally Mixed Confluent Nozzle Related to Excited Core-Jet Instability;AIAA AVIATION 2023 Forum;2023-06-08
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