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Experimental investigation of boundary-layer transition on a cooled 7.5 deg total-angle cone at mach 10
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1967 |
| Description | Boundary layer transition for cooled 7.5 deg total angle cone at Mach 10 |
| File Size | 2610370 |
| Page Count | 37 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19670029031 |
| Archival Resource Key | ark:/13960/t42r8kc7g |
| Language | English |
| Publisher Date | 1967-10-01 |
| Access Restriction | Open |
| Subject Keyword | Heat Transfer Boundary Layer Transition Hypersonic Speed Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |