Investigation of the Flow over a Spiked-Nose Hemisphere Cylinder at a Mach Number of 6.8. Crawford, D., H. Technical Report NASA, 1959.
bibtex   
@techreport{
 title = {Investigation of the Flow over a Spiked-Nose Hemisphere Cylinder at a Mach Number of 6.8},
 type = {techreport},
 year = {1959},
 institution = {NASA},
 revision = {Technical Note D-118},
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 created = {2021-07-12T05:21:20.996Z},
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 last_modified = {2021-07-12T05:21:20.996Z},
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 citation_key = {crawford:nasa:1959},
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 bibtype = {techreport},
 author = {Crawford, Davis H.}
}

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