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Afterburner performance with combustion-chamber lengths from 10 to 62 inches at several afterburner-inlet temperatures (Document No: 19650018859)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1956 |
| Description | Effect of variation of combustion chamber length and inlet temperature on low pressure-loss sea level afterburner |
| File Size | 711442 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650018859 |
| Archival Resource Key | ark:/13960/t5hb3vd23 |
| Language | English |
| Publisher Date | 1956-02-01 |
| Access Restriction | Open |
| Subject Keyword | Afterburner Air Inlet Combustion Chamber 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 |