A Wind Tunnel Experiment for Symmetric Wakes in Adverse Pressure Gradients
Author:
Affiliation:
1. Technical University of Braunschweig
2. German Aerospace Center (DLR)
3. Peter the Great St. Petersburg Polytechnic University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1875
Reference17 articles.
1. Prediction of high lift: review of present CFD capability
2. Investigation of Confluent Boundary Layers in High-Lift Flows
3. Investigation of scaling laws in a turbulent boundary layer flow with adverse pressure gradient using PIV
4. Gungor, A. G., Maciel, Y., Simens, M. P., Soria, J.: Analysis of a Turbulent Boundary Layer Subjected to aStrong Adverse Pressure Gradient. Journal of Physics: Conference Series 5060, pp.12007, 2014.
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1. Study of RANS Turbulence Models for Turbulent Wake Flow in Adverse Pressure Gradient;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2021
2. LES-based Computation of Evolution of Turbulent Wakes Subjected to Adverse Pressure Gradient;Mathematical Models and Computer Simulations;2021-01
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