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 /
| Main Author: | |
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| Format: | Government Document eBook |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration,
August 1969.
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| Series: | NASA technical memorandum ;
X-1840. |
| Subjects: | |
| Online Access: | https://purl.fdlp.gov/GPO/gpo182864 |