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Cold flow investigation of a low angle turbojet plug nozzle with fixed throat and translating shroud at mach numbers from 0 to 2.0
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1968 |
| Description | Cold flow tests of aerodynamic characteristics of plug nozzle configuration for turbojet engines operating at supersonic speeds |
| File Size | 9218189 |
| Page Count | 38 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19680020481 |
| Archival Resource Key | ark:/13960/t1dk05s7d |
| Language | English |
| Publisher Date | 1968-08-01 |
| 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 |