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Performance characteristics of an isolated coannular plug nozzle at transonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mercer, C. E. Burley II, J. R. |
| Copyright Year | 1985 |
| Description | The Langley 16-Foot Transonic Tunnel was used to evaluate the performance characteristics of a coannular plug nozzle at static conditions (Mach number of 0) and at Mach numbers from 0.65 to 1.20. Jet total pressure ratio was varied from 1.0 (jet off) to 10.0. Thirty-seven configurations generated by the combination of three geometric variables - plug angle, shroud boattail length (fixed exit radius), and shroud extension length - were tested. |
| File Size | 6555988 |
| Page Count | 152 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860008822 |
| Archival Resource Key | ark:/13960/t2r54hj6p |
| Language | English |
| Publisher Date | 1985-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Nozzle Geometry Plug Nozzles Performance Tests Shrouded Nozzles Boattails Annular Nozzles Jet Blast Effects Pressure Ratio Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
