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Experimental performance of a 0.35 hub-tip radius ratio transonic axial-flow-compressor stage designed for 40 pounds per second per unit frontal area
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1958 |
| File Size | 1970238 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930090120 |
| Archival Resource Key | ark:/13960/t5k97x76d |
| Language | English |
| Publisher Date | 1958-09-04 |
| Access Restriction | Open |
| Subject Keyword | 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 |