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Effects of internal-area distribution, spike translation, and throat boundary-layer control on performance of a double-cone axisymmetric inlet at mach numbers from 3.0 to 2.0
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1957 |
| File Size | 17762639 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930089784 |
| Archival Resource Key | ark:/13960/t84j5765n |
| Language | English |
| Publisher Date | 1957-08-30 |
| Access Restriction | Open |
| Subject Keyword | 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 |