Search results

|area=2 ...<b>Table CFD&nbsp;&ndash;&nbsp;A&nbsp;&nbsp;</b>Summary description of all test cases

'''Application Challenge 6-07''' <font size="-2" color="#888888">               © copyright ERCOFTAC 2004</font> | style="width: 2.0cm; border-top: none; border-left: none; border-bottom: solid windowtext 1

{{AC|front=AC 4-01|description=Description_AC4-01|testdata=Test Data_AC4-01|cfdsimulations=CFD Simulations_AC4-01|evaluation=Evaluation_AC4 ...cross-section (Snyder, 1981). In this case, the terminal building is only 2.5% of the tunnel cross-section and thus tunnel wall effects could be ignore

...nolds number in the experiments, due to the reasons discussed in section [[Test Data AC7-02#Measurement errors|Measurement errors]]. 1. '''Computational meshes''': LES1&2 employ the same comp. meshes, whereas LES3 and RANS use different meshes.

The measured mean velocity at the inlet of the model, shown in [[Test Data AC7-02#Figure7|figure 7]], is asymmetric, probably due to the action o ...le Navier-Stokes equations. ''Journal of Computational Physics'' '''59''' (2), 308&nbsp;&ndash;&nbsp;323.