Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignment of the rotor blade for zero angle of attack
| Author: | Stanitz, John D |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2986 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56779/ |