Aerodynamic performance of several techniques for spike-position control of a blunt-lip nose inlet having internal contraction; Mach numbers of 0.63 and 1.5 to 2.0
| Author: | Anderson, Arthur A |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E57D15 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63487/ |