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Effect of boundary-layer control and inlet lip shape on the performance of a twin-scoop air-induction system at mach numbers from 0 to 1.9
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1956 |
| File Size | 23033998 |
| Page Count | 53 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930089049 |
| Archival Resource Key | ark:/13960/t1tf4hz1r |
| Language | English |
| Publisher Date | 1956-02-14 |
| 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 |