Investigation of lift and center of pressure of low-aspect-ratio, cruciform, triangular, and rectangular wings in combination with a slender fuselage at high supersonic speeds
| Author: | Canning, Thomas N |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A52C24 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59278/ |