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Pressure distribution of a 0.0667-scale model of the x-15 airplane for an angle-of-attack range of 0 deg to 28 deg at mach numbers of 2.30, 2.88, and 4.65
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1960 |
| Description | Pressure distribution on x-15 aircraft model |
| File Size | 105977618 |
| Page Count | 164 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630002770 |
| Archival Resource Key | ark:/13960/t7np6sr05 |
| Language | English |
| Publisher Date | 1960-05-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution X-15a Aircraft Aircraft Model Aerodynamics Yaw Wind Tunnel Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |