Comparison of airfoil sections on two triangular-wing-fuselage configurations at transonic speeds from tests by the NACA wing-flow method
| Author: | Hall, Albert W. |
|---|---|
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L51F01 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59009/ |