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Flow-field investigations on the x-15 airplane and model up to hypersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1968 |
| Description | Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraft |
| File Size | 1542507 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19680025701 |
| Archival Resource Key | ark:/13960/t3mw75v5h |
| Language | English |
| Publisher Date | 1968-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |