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Static performance of an auxiliary inlet ejector nozzle for supersonic-cruise aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1968 |
| Description | Static performance of an auxiliary inlet ejector nozzle for supersonic-cruise aircraft |
| File Size | 12428514 |
| Page Count | 42 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19680026292 |
| Archival Resource Key | ark:/13960/t3518rc0k |
| Language | English |
| Publisher Date | 1968-10-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems 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 |