A Rapid Graphical Method for Computing the Pressure Distribution at Supersonic Speeds on a Slender Arbitrary Body of Revolution
| Author: | Thompson, Jim Rogers |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-1768 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55019/ |