Adaptive Finite Volume Upwind Approaches for Aeroacoustic Computations
Author:
Affiliation:
1. National Cheng Kung University, Tainan, Taiwan 70101, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.259
Reference19 articles.
1. Computational Study on the Interaction Between a Vortex and a Shock Wave
2. Using high-order accurate essentially nonoscillatory schemes for aeroacoustic applications
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5. Unstructured adaptive mesh computations of rotorcraft high-speed impulsive noise
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