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Effect of chamber-to-nozzle heat exchange on frozen and equilibrium flows in de laval nozzles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1970 |
| Description | Determining exit conditions that result when heat is withdrawn from rocket thrust chamber and added to gas flow in nozzle |
| File Size | 2907950 |
| Page Count | 124 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19700019358 |
| Archival Resource Key | ark:/13960/t4mm12v9f |
| Language | English |
| Publisher Date | 1970-04-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics 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 |