Implicit Large-Eddy Simulation of Swept-Wing Flow Using High-Resolution Methods
Author:
Affiliation:
1. Cranfield University, Cranfield, England MK43 0EB, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.37806
Reference34 articles.
1. Computational challenges in high angle of attack flow prediction
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3. Compact Difference Scheme Applied to Simulation of Low-Sweep Delta Wing Flow.
4. High-Order Simulation of Low Sweep Delta Wing Flows Using a Hybrid RANS/ILES Model
5. Numerical simulation of the interaction between a leading-edge vortex and a vertical tail
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