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JAXA Repository AIREX: Pressure Gradient Effects on Transition Location over Axisymmetric Bodies at Incidence in Supersonic Flow: Progress Report of JAXANASA Joint Research Project on Supersonic Boundary Layer Transition Part 2

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Figure 1. Geometry of selected axisymmetric shapes [4].
Table 1: Summary of flow conditions and case notation.  Geometric Configuration  Flow Condition
Figure 3. Mean velocity profiles  along the leeward ray [1-4]. (a) SC5-0deg-99(a) SC5-0deg-99
Figure 2. Surface pressure  distribution [1-4].
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