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Experimental investigation of the turbulent boundary layer at a mach number of 6 with heat transfer at high reynolds numbers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1967 |
| Description | Turbulent boundary layer skin friction and heat transfer on hollow cylinder in hypersonic flow at high Reynolds numbers |
| File Size | 3121955 |
| Page Count | 76 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19670010557 |
| Archival Resource Key | ark:/13960/t6sz11t4q |
| Language | English |
| Publisher Date | 1967-03-01 |
| Access Restriction | Open |
| Subject Keyword | Cylindrical Shell Hypersonic Flow Skin Friction Heat Transfer Turbulent Boundary Layer 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 |