Effect of liner air-entry holes, fuel state, and combustor size on performance of an annular turbojet combustor at low pressures and high air-flow rates
| Author: | Norgren, Carl T. |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E52J09 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59474/ |