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Flow field survey and decelerator drag characteristics in the wake of a model of the x-15 airplane at mach 2.30 and 4.65
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1966 |
| Description | Flow field survey and decelerator drag characteristics in wake of model X-15 airplane at Mach 2.30 and 4.65 |
| File Size | 2201124 |
| Page Count | 38 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660007274 |
| Archival Resource Key | ark:/13960/t9x10v16p |
| Language | English |
| Publisher Date | 1966-02-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Flow Field Deceleration X-15 Aircraft 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 |