Aerodynamic characteristics of a 6-percent-thick symmetrical circular-arc airfoil having a 30-percent-chord trailing-edge flap at a Mach number of 6.9
| Author: | Ridyard, Herbert W |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56B24 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62279/ |