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Oliver, Robert E. (1957) Part I. The effect of a simple throat distortion on the downstream flow in a hypersonic wind tunnel nozzle. Part II. An experimental investigation of flow over simple blunt bodies at a nominal Mach number of 5.8. Engineer's thesis, California Institute of Technology. doi:10.7907/462P-XC43. https://resolver.caltech.edu/CaltechETD:etd-07152004-105812

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