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Investigation of a mixed-compression axisymmetric inlet system at mach numbers 0.6 to 3.5
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1970 |
| Description | Wind tunnel tests of mixed compression axisymmetric inlet system at Mach numbers 0.6 to 3.5 |
| File Size | 8034194 |
| Page Count | 247 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19710003549 |
| Archival Resource Key | ark:/13960/t1tf4jn4k |
| Language | English |
| Publisher Date | 1970-11-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems 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 |