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Wind-Tunnel Investigation at a Mach Number of 2.01 of the Aerodynamic Characteristics in Combined Angles of Attack and Sideslip of Several Hypersonic Missile Configurations with Various Canard Controls
| Author: | Robinson, Ross B. |
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| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L58A21 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc52987/ |
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