Effect of leading-edge chord-extensions on the aerodynamic characteristics of a 45 degree sweptback wing-fuselage combination at Mach numbers of 0.40 to 1.03
| Author: | West, F. E., Jr. |
|---|---|
| Additional Authors: | Martz, Gladys S. |
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53B02 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59557/ |
