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Oliver, Robert Earl (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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