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Preliminary investigation of a rectangular supersonic scoop inlet with swept sides designed for low drag at a mach number of 2.7
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1952 |
| File Size | 28549509 |
| Page Count | 66 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930087347 |
| Archival Resource Key | ark:/13960/t9r259177 |
| Language | English |
| Publisher Date | 1952-11-26 |
| 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 |