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Cooling characteristics of an experimental tail-pipe burner with an annular cooling-air passage (Document No: 19660010444)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1952 |
| Description | Tail-pipe fuel ratio, mass flow of combustion gas, and radial fuel flow distribution on cooling requirements of tail-pipe burner with annular cooling-air passage |
| File Size | 10169600 |
| Page Count | 63 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660010444 |
| Archival Resource Key | ark:/13960/t0ms82j48 |
| Language | English |
| Publisher Date | 1952-02-26 |
| Access Restriction | Open |
| Subject Keyword | Combustion Mass Flow Burner Temperature Profile Cooling 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 |