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Investigation of the flow through a single-stage two-dimensional nozzle in the langley 11-inch hypersonic tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 17359026 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082869 |
| Archival Resource Key | ark:/13960/t6158xh3v |
| Language | English |
| Publisher Date | 1950-12-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Tests - Naca - Hypersonic (11") Nozzles, High-pressure Flow - Nozzles Wind Tunnels - Air Flow Wind Tunnel Apparatus - Naca - Hypersonic (11") Wind Tunnels - Pressure 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 |