Investigation of the aerodynamic characteristics of the NACA RM-10 missile (with fins) at a Mach number of 1.62 in the Langley 9-inch supersonic tunnel
| Author: | Coletti, Donald E. |
|---|---|
| Year: | 1952 |
| Document Type: | NACA |
| Issuing Agency: | National Advisory Committee for Aeronautics, |
| SUDOC: | Y 3.N21/5:15/L52J23a |
| Series: | National Advisory Committee for Aeronautics research memorandum ; |
| Report Number: | L52J23a |
| Subjects: | Aerodynamics, Supersonic |
| Guided missiles--Aerodynamics | |
| Link: | https://hdl.handle.net/2027/mdp.39015086465138 |
