Attempt to Evaluate the Computations for Test Case 6.1 - Cold Hypersonic Flow Past Ellipsoidal Shapes -
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The laminar flow past ellipsoidal shapes, see figure 1, was chosen most often as test case, and more than 20 groups have presented results for such flows at the Antibes workshop. The present attempt to evaluate the different computational contributions for cold hypersonic flows is based on the contributions to the proceedings, and, in particular, on those numerical data which were provided in discrete form by contributors to the first author. Seventeen contributions have been received associated with test case 6.1: eight of these contributions deal with two-dimensional flows only (6.1-1 to 6.1-4) and four are only for three-dimensional simulations (6.1-5 to 6.1-8), see table 1. The request for field data was not followed, in general, so that wall values are used for comparison purpose.