Loading...
Please wait, while we are loading the content...
Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1959 |
| Description | Overall stage and stator blade element performance with straight stator and tilted stator in transonic axial flow compressor stage |
| File Size | 7282012 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650003088 |
| Archival Resource Key | ark:/13960/t14n3x48t |
| Language | English |
| Publisher Date | 1959-10-01 |
| Access Restriction | Open |
| Subject Keyword | Stator Blade Transonic Flow Axial Flow Compressor 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 |