Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
| Author: | Love, Eugene S. |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Technical Reports |
| Report Number: | NACA-TR-1238 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc65577/ |