The effects of suction through porous leading-edge surfaces on the aerodynamic characteristics of a 47.5 degree sweptback wing-fuselage combination at a Reynolds number of 4.4 x 10(exp 6)
| Author: | Scallion, William I. |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L51K15 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59855/ |