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Experimental investigation of an axial-flow supersonic compressor having sharp leading-edge blades with an 8-percent mean thickness chord ratio
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1955 |
| File Size | 2193699 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930088382 |
| Archival Resource Key | ark:/13960/t3dz4zw2q |
| Language | English |
| Publisher Date | 1955-02-04 |
| Access Restriction | Open |
| Subject Keyword | 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 |