Boundary-Layer Stability Analysis of the Mean Flows Obtained Using Unstructured Grids
Author:
Affiliation:
1. Corvid Technologies, National Institute of Aerospace, Hampton, Virginia 23666
2. Computational AeroSciences Branch, 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/10.2514/1.C032583
Reference30 articles.
1. ChangC.L. “The Langley Stability and Transition Analysis Code (LASTRAC): LST, Linear and Nonlinear PSE for 2-D, Axisymmetric, and Infinite Swept Wing Boundary Layers,” AIAA Paper 2003-0974, 2003.
2. ChangC.L. “LASTRAC.3d: Transition in 3D Boundary Layers,” AIAA Paper 2004-2542, 2004.
3. Boundary-Layer Receptivity and Integrated Transition Prediction
4. An implicit upwind algorithm for computing turbulent flows on unstructured grids
5. Implicit/Multigrid Algorithms for Incompressible Turbulent Flows on Unstructured Grids
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