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Local turbulent skin-friction measurements on a flat plate at mach numbers from 2.5 to 4.5 and reynolds numbers up to 69 x 106
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1965 |
| Description | Supersonic wind tunnel tests of turbulent skin friction on flat plate at very high Reynolds number |
| File Size | 788945 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650018215 |
| Archival Resource Key | ark:/13960/t3mw75m6v |
| Language | English |
| Publisher Date | 1965-07-01 |
| Access Restriction | Open |
| Subject Keyword | Reynolds Number Skin Friction Supersonic Wind Tunnel Flat Plate 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 |