An experimental investigation of four triangular-wing-body combinations in sideslip at Mach numbers 0.6, 0.9, 1.4, and 1.7
| Author: | Christensen, Frederik B. |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A53L22 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59957/ |