Investigation of the Flow over a Spiked-Nose Hemisphere Cylinder at a Mach Number of 6.8. Crawford, D. H. Technical Report 1959.
bibtex   
@techreport{crawford1959,
	title = {Investigation of the {Flow} over a {Spiked}-{Nose} {Hemisphere} {Cylinder} at a {Mach} {Number} of 6.8},
	author = {Crawford, Davis H.},
	year = {1959},
}

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