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Nonsteady-flow thrust augmenting ejectors
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Foa, J. V. |
| Copyright Year | 1979 |
| Description | Ejector augmenters in which the transfer of mechanical energy from the primary to the secondary flow takes place through the work of interface pressure forces are investigated. Nonsteady flow processes are analyzed from the standpoint of energy transfer efficiency and a comparison of a rotary jet augmenter to an ejector is presented. |
| File Size | 505055 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800001878 |
| Archival Resource Key | ark:/13960/t3nw48f61 |
| Language | English |
| Publisher Date | 1979-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Nozzle Design Steady Flow Ejectors Thrust Augmentation Pressure Distribution Unsteady Flow Energy Transfer Nozzle Efficiency Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |