Determination of Turbofan Inlet Acoustics Using Finite Elements
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Ga.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61020
Reference23 articles.
1. The acoustics of aircraft engine-duct systems
2. A finite difference method for computing sound propagation in nonuniform ducts
3. Predicting the acoustic properties of arbitrarily shaped bodies by use of an integral approach
4. Transmission of spinning acoustic modes in a slightly non-uniform duct
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1. FINITE ELEMENT MODELING OF ACOUSTICS USING HIGHER ORDER ELEMENTS PART II: TURBOFAN ACOUSTIC RADIATION;Journal of Computational Acoustics;2004-09
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5. Coupling of Boundary and Finite Elements in Aeroacoustic Calculations;Notes on Numerical Fluid Mechanics (NNFM);1995
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