Wind-Tunnel Investigation at a Mach Number of 2.01 of Forebody Strakes for Improving Directional Stability of Supersonic Aircraft
| Author: | Driver, Cornelius |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L58C11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64072/ |