An iterative finite element-integral technique for predicting sound radiation from turbofan inlets in steady flight

DOI10.2514/3.9429zbMath0617.76093OpenAlexW1994881382MaRDI QIDQ3754357

Scott J. Horowitz, Ben T. Zinn, Robert K. Sigman

Publication date: 1986

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.9429

zbMATH Keywords

finite element methodsound fieldcontinuous solutioniterative solution techniqueintegral solutionsturbofan inletintegral solution techniquesteady flight

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05) Basic methods in fluid mechanics (76M99)

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