An iterative finite element-integral technique for predicting sound radiation from turbofan inlets in steady flight
- 1 August 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 24 (8) , 1256-1262
- https://doi.org/10.2514/3.9429
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
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