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Experimental investigation at mach numbers from 0 to 1.9 of trapezoidal and circular side inlets for a fighter-type airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1955 |
| File Size | 18465793 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930088691 |
| Archival Resource Key | ark:/13960/t0ms8fn5n |
| Language | English |
| Publisher Date | 1955-07-28 |
| Access Restriction | Open |
| Subject Keyword | 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 |