The Drag of Finite-Length Cylinders Determined From Flight Tests at High Reynolds Numbers for a Mach Number Range From 0.5 to 1.3
| Author: | Welsh, Clement J. |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2941 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56717/ |