Numerical study on radiation of multiple pure tone noise from an aircraft engine inlet
- 10 May 1999
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Generalized formulation and application of characteristic boundary conditionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Supersonic fan tone noise predictionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Dispersion-Relation-Preserving Finite Difference Schemes for Computational AcousticsJournal of Computational Physics, 1993
- A flight study of tone radiation patterns generated by inlet rods ina small turbofan enginePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- A note on multiple pure tone noiseJournal of Sound and Vibration, 1971
- Multiple tone generation by transonic compressorsJournal of Sound and Vibration, 1971