Number of items:
1
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O'Bryant, William Theral
(1956)
An Experimental Investigation of Hypersonic Flow over Blunt Nosed Cones at a Mach Number of 5.8.
Engineer's thesis, California Institute of Technology.
doi:10.7907/923A-XB12.
https://resolver.caltech.edu/CaltechETD:etd-06182004-111807
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