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Internal performance of a series of circular auxiliary-air inlets immersed in a turbulent boundary layer : mach number range: 1.5 to 2.0
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1955 |
| File Size | 16984809 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930088569 |
| Archival Resource Key | ark:/13960/t1xd5mk7x |
| Language | English |
| Publisher Date | 1955-03-03 |
| 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 |