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Performance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1969 |
| Description | Evaluating performance of swirl can turbojet combustor at simulated supersonic inlet conditions |
| File Size | 7334599 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19690006822 |
| Archival Resource Key | ark:/13960/t1ck34z4m |
| Language | English |
| Publisher Date | 1969-01-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems 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 |