Experimental Investigation of the Aerodynamic Characteristics of an Air-to-Air Missile Employing Cruciform Wings and Tail of Rectangular Plan Form at Mach Numbers of 1.4 and 1.9
| Author: | Mead, Merrill H. |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A52K14 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59483/ |