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Analysis of limitations imposed on one-spool turbojet-engine designs by compressors and turbines at flight mach numbers of 0, 2.0, and 2.8
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1954 |
| File Size | 2601107 |
| Page Count | 51 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930088284 |
| Archival Resource Key | ark:/13960/t4wh6zp0z |
| Language | English |
| Publisher Date | 1954-09-24 |
| 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 |