Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips: Subsonic leading edges and supersonic trailing edges
| Author: | Hannah, Margery E. |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2831 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56388/ |