Effect of leading-edge droop on the aerodynamic and loading characteristics of a 4-percent-thick unswept-wing-fuselage combination at transonic speeds
| Author: | Schmeer, James W |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56C14 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62188/ |