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Effect of angle of attack and injection pressure on jet penetration and spreading from a delta wing in supersonic flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1969 |
| Description | Effect of angle of attack and injection pressure on jet penetration and spreading from delta wing in supersonic flow |
| File Size | 11074429 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19690027893 |
| Archival Resource Key | ark:/13960/t45q9p65g |
| Language | English |
| Publisher Date | 1969-09-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |