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Investigation of boundary-layer transition on 10 degree cone in langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.41, 1.61, and 2.01
| Author: | Sinclair, Archibald R |
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| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3648 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55938/ |
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