An experimental investigation of flow over simple blunt bodies at a mach number of 5.8
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document. Shock stand-off distances and shock shapes were measured and/or observed for a series of 14 blunt-nosed bodies at a Mach number of 5. 8 and Reynolds number per inch of [...]. Nine of...
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