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Flow field for an underexpanded, supersonic nozzle exhausting into an expansive launch tube
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Batson, J. L. Bertin, J. J. Morris, R. R. |
| Copyright Year | 1976 |
| Description | Static pressure distributions along the launcher wall and pitot pressure measurements from the annular region between the rocket and the launcher were made as an underexpanded supersonic nozzle exhausted into an expansive launch tube. The flow remained supersonic along the entire length of the launcher for all nozzle locations studied. |
| File Size | 351054 |
| Page Count | 7 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770003433 |
| Archival Resource Key | ark:/13960/t23c0tr8q |
| Language | English |
| Publisher Date | 1976-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Rocket Nozzles Static Pressure Shock Waves Mass Flow Rate Supersonic Nozzles Flow Distribution Pitot Tubes Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
