Effects of Internal-Area Distribution, Spike Translation, and Throat Boundary-Layer Control on Performance of a Double-Cone Axisymmetric Inlet at Mach Numbers From 3.0 to 2.0
| Author: | Connors, James F. |
|---|---|
| Additional Authors: | Lovell, J. Calvin |
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E57F03 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63620/ |