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Performance characteristics at mach numbers to 2.0 of various types of side inlets mounted on fuselage of proposed supersonic airplane ii : inlets utilizing half of a conical spike
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1952 |
| File Size | 25190220 |
| Page Count | 52 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930087308 |
| Archival Resource Key | ark:/13960/t1jh7wp9x |
| Language | English |
| Publisher Date | 1952-09-04 |
| 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 |