Results of flight tests to determine the drag of finite-length cylinders at high Reynolds numbers for a Mach number range of 0.5 to 1.3
| Author: | Welsh, Clement J |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52C31 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59361/ |