CORE ENGINE NOISE CONTROL PROGRAM. VOLUME III. PREDICTION METHODS
Prediction methods for core engine noise were reviewed and either updated or new noise evaluation techniques formulated for low velocity coannular jets, combustors ('core' noise), Low pressure turbines, interaction between turbine tones and fan/core jet streams, obstructions in the flow passages and casing radiation. The development was based, to a large extent, on the analytical investigation and the model, component and engine tests evaluated during Phases 2 and 3 of this program. The results were cast in a general form, so as to be applicable to a wide variety of cycles, including present and future turbofan engines. The prediction methods were validated with measured acoustic data wherever possible.
- See also Volume 2, AD-A013 129.
General ElectricMarine Turbine & Gear Engineer, 1100 Western Ave
Lynn, MA United States 01910
Washington, DC United States
- Kazin, S B
- Matta, R K
- Bilwakesh, K R
- Emmerling, J J
- Latham, D
- Publication Date: 1974-8
- Pagination: 179 p.
- TRT Terms: Acoustic measuring instruments; Acoustics; Aircraft noise; Civil aircraft; Engine components; Jet engines; Noise; Noise control; Turbofan engines
- Uncontrolled Terms: Noise reduction
- Old TRIS Terms: Acoustic measurement; Jet engine noise
- Subject Areas: Aviation; Environment; Vehicles and Equipment;
- Accession Number: 00092128
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: Final Rpt., FAA-RD-74-125-3
- Contract Numbers: DOT-FA72WA-3023
- Files: NTIS, USDOT
- Created Date: Oct 18 1976 12:00AM