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A mixing model for rocket engine combustion
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1965 |
| Description | Model for prediction of rocket engine combustion with performance parameters of gas phase turbulent diffusion, and mixing of oxidizer and fuel vapors |
| File Size | 1248778 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650017000 |
| Archival Resource Key | ark:/13960/t5k97xg90 |
| Language | English |
| Publisher Date | 1965-06-01 |
| Access Restriction | Open |
| Subject Keyword | Rocket Engine Oxidizer Gas Phase Combustion 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 |