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...UFR 2-04 Description|references=UFR 2-04 References|testcase=UFR 2-04 Test Case|evaluation=UFR 2-04 Evaluation|qualityreview=UFR 2-04 Quality Review|bestpr ...e) it would be of great value to continue the numerical study of this test case with such models of turbulence for closure, so as to update the assessment

= Test Case = == Brief Description of the Study Test Case ==

...UFR 2-04 Description|references=UFR 2-04 References|testcase=UFR 2-04 Test Case|evaluation=UFR 2-04 Evaluation|qualityreview=UFR 2-04 Quality Review|bestpr = Test Case =

...UFR 2-07 Description|references=UFR 2-07 References|testcase=UFR 2-07 Test Case|evaluation=UFR 2-07 Evaluation|qualityreview=UFR 2-07 Quality Review|bestpr ...Rotor 37 is flawed due to a hub leakage [2], Rotor 67 was chosen for this study. Transonic, three-dimensional flows represent severe challenges for any num

...UFR 1-02 Description|references=UFR 1-02 References|testcase=UFR 1-02 Test Case|evaluation=UFR 1-02 Evaluation|qualityreview=UFR 1-02 Quality Review|bestpr = Test Case =

The turbulent Channel Flow is one of the canonical flows used to study turbulence in wall bounded turbulence. DNS of turbulent channel flow were u Turbulent channel has been one of the canonical test cases to study the characteristics of wall bounded turbulence.

...UFR 4-06 Description|references=UFR 4-06 References|testcase=UFR 4-06 Test Case|evaluation=UFR 4-06 Evaluation|qualityreview=UFR 4-06 Quality Review|bestpr = Test Case =

...UFR 2-03 Description|references=UFR 2-03 References|testcase=UFR 2-03 Test Case|evaluation=UFR 2-03 Evaluation|qualityreview=UFR 2-03 Quality Review|bestpr ...aspect ratio to ensure good shock capturing during the shock movement. (A study is recommended).

...vior was measured for Mach~1.35 which is the “strong” case. For the “weak” case, Mach~1.25, the boundary layer remains attached along the diverging part of

...UFR 4-05 Description|references=UFR 4-05 References|testcase=UFR 4-05 Test Case|evaluation=UFR 4-05 Evaluation|qualityreview=UFR 4-05 Quality Review|bestpr ...ondary flows will be weak compared to decelerating flow. Furthermore, this study will mainly focus on the influence of the mesh and the turbulence model ont

...ption=UFR_2-02_Descr|references=UFR 2-02 References|testcase=UFR 2-02 Test Case|evaluation=UFR 2-02 Evaluation|qualityreview=UFR 2-02 Quality Review|bestpr ...h circular and square cross sections are considered; the actual study test case will be the flow around a square cylinder.

already quite complex due to the unsteady vortex shedding, but in the case of finite-height ...kness of the approach flow ''δ/h'' are the parameters in the finite-height case.

...UFR 3-06 Description|references=UFR 3-06 References|testcase=UFR 3-06 Test Case|evaluation=UFR 3-06 Evaluation|qualityreview=UFR 3-06 Quality Review|bestpr = Test Case =

The present case consists of the flow through a wall bounded pin matrix in a staggered arran In addition to its interest for the complex underlying physics, this case is close to several industrial configurations found in internal cooling of

Our aim in the present test-case is to predict the following physical parameters: ...tion scheme. For High fidelity results, the finer mesh used in the present study is necessary.

...UFR 3-03 Description|references=UFR 3-03 References|testcase=UFR 3-03 Test Case|evaluation=UFR 3-03 Evaluation|qualityreview=UFR 3-03 Quality Review|bestpr = Test Case =

...most of the contributions focus on a certain part of the flow. The present study published in Wood et al. (2016) includes experimental investigations and la ...around hemispheres at a sub-critical Reynolds number of Re = 140,000. The study included different turbulent boundary layers classified in thin, smooth and

interesting area of research is the experimental and computational study of compressible The test case investigated in the current contribution under the framework of the

...UFR 3-05 Description|references=UFR 3-05 References|testcase=UFR 3-05 Test Case|evaluation=UFR 3-05 Evaluation|qualityreview=UFR 3-05 Quality Review|bestpr = Test Case =

...UFR 2-05 Description|references=UFR 2-05 References|testcase=UFR 2-05 Test Case|evaluation=UFR 2-05 Evaluation|qualityreview=UFR 2-05 Quality Review|bestpr 4. A. Jirásek, P.Eliasson and S Wallin (2001a). “Computational Study of the High-Lift A-airfoil”. AIAA 2001-0708