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Effect of hypersonic research engine installation on aerodynamic characteristics of 0.0667-scale model of x-15a-2 airplane at mach numbers from 1.75 to 4.63
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1969 |
| Description | Wind tunnel stability tests to determine effect of hypersonic research engine on aerodynamic characteristics of research aircraft |
| File Size | 348209059 |
| Page Count | 188 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19690029227 |
| Archival Resource Key | ark:/13960/t1wd8mc4m |
| Language | English |
| Publisher Date | 1969-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |