Using high-order accurate essentially nonoscillatory schemes for aeroacoustic applications
Author:
Affiliation:
1. ViGYAN, Inc., Hampton, Virginia 23666
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13057
Reference11 articles.
1. Uniformly high order accurate essentially non-oscillatory schemes, III
2. Efficient implementation of essentially non-oscillatory shock-capturing schemes
3. A numerical study of the convergence properties of ENO schemes
4. Numerical experiments on the accuracy of ENO and modified ENO schemes
5. High-order ENO methods for the unsteady compressible Navier-Stokes equations
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1. Aeroacoustic Computations Using a High-Order Shock-Capturing Scheme;AIAA Journal;2007-10
2. Aeroacoustic Computations Using a High Order Shock Capturing Scheme;12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference);2006-05-08
3. One-Step Aeroacoustics Simulation Using Lattice Boltzmann Method;AIAA Journal;2006-01
4. Multi-size-mesh Multi-time-step Dispersion-relation-preserving Scheme for Multiple-scales Aeroacoustics Problems;International Journal of Computational Fluid Dynamics;2003-03
5. Computation of Shock-Sound Interaction Using Finite Volume Essentially Nonoscillatory Scheme;AIAA Journal;2002-06
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