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Experimental investigation of effects of combustion-chamber length and inlet total temperature, total pressure, and velocity on afterburner performance (Document No: 19630006360)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1957 |
| Description | Afterburner combustion efficiency - effects of chamber length, temperature, pressure and velocity |
| File Size | 6939114 |
| Page Count | 79 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630006360 |
| Archival Resource Key | ark:/13960/t4zh1c46c |
| Language | English |
| Publisher Date | 1957-06-03 |
| Access Restriction | Open |
| Subject Keyword | Combustion Efficiency Chamber Pressure Afterburner 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 |