Effects of Components and Various Modifications on the Drag and the Static Stability and Control Characteristics of a 42 Deg Swept-Wing Fighter-Airplane Model at Mach Numbers of 1.60 to 2.50
| Author: | Church, James D. |
|---|---|
| Year: | 1959 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L57K01 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc53080/ |