Global Stability Analysis of a Compressible Turbulent Flow Around a High-Lift Configuration
Author:
Affiliation:
1. Airbus Operations S.L., 28906 Getafe, Spain
2. Universidad Politécnica de Madrid, 28004 Madrid, Spain
3. Airbus Group Innovations, Filton, England BS3 47QW, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054211
Reference27 articles.
1. High-Lift Aerodynamics
2. Prediction of high lift: review of present CFD capability
3. Two-dimensional global low-frequency oscillations in a separating boundary-layer flow
4. On the dynamics of axisymmetric turbulent separating/reattaching flows
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