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Experimental investigation of a turbulent boundary layer at mach 6, high reynolds numbers, and zero heat transfer
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1965 |
| Description | Turbulent boundary layer on hollow cylinder at Mach 6, high Reynolds number, and zero heat transfer |
| File Size | 5244824 |
| Page Count | 60 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650020242 |
| Archival Resource Key | ark:/13960/t59d1pc8j |
| Language | English |
| Publisher Date | 1965-06-01 |
| Access Restriction | Open |
| Subject Keyword | Turbulent Boundary Layer Heat Transfer Cylinder Reynolds Number Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |