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JAXA Repository AIREX: Pressure Gradient Effects on Mean Flow over Axisymmetric Bodies at Incidence in Supersonic Flow: Progress Report of JAXANASA Joint Research Project on Supersonic Boundary Layer Transition Part 1

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Figure 1.    Geometry of selected axisymmetric shapes.
Table 1: Summary of flow conditions and case notation.
Table 2: Summary of numerical grid
Figure 2.  Typical JAXA-grid of the SC5 configuration.
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