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Investigation of a high-flow transonic-compressor inlet stage having a hub-tip radius ratio of 0.35
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1958 |
| File Size | 19216925 |
| Page Count | 49 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930089843 |
| Archival Resource Key | ark:/13960/t2q57b70h |
| Language | English |
| Publisher Date | 1958-03-06 |
| 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 |