Flight study of induced turbofan inlet acoustic radiation with theoretical comparisons
- 1 January 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (1) , 57-62
- https://doi.org/10.2514/3.45080
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Flight effects on fan noise with static and wind tunnel comparisonsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Wave envelope and infinite element schemes for fan noise radiation from turbofan inletsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Experimental investigation of geometry and flow effects on acoustic radiation from duct inletsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- An iterative finite element-integral technique for predicting sound radiation from turbofan inlets in steady flightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Analysis of radiation patterns of interaction tones generated by inlet rods in the JT15D enginePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Modal propagation angles in a cylindrical duct with flow and their relation to sound radiationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979