Effect of camber and twist on the stability characteristics of models having a 45 degree swept wing as determined by the free-fall method at transonic speeds
| Author: | White, Maurice D |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A52F16 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59286/ |