Wall-Resolved Large-Eddy Simulations of Transonic Shock-Induced Flow Separation
Author:
Affiliation:
1. National Institute of Aerospace, Hampton, Virginia 23666
2. NASA Langley Research Center, Hampton, Virginia 23681
Funder
Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057850
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4. Application of a Lattice-Boltzmann Method to the Separated Flow over the NASA Hump
5. Wall--modeled Large Eddy Simulation of Flow Over a Wall--mounted Hump
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