Influence of a canard-type control surface on flow field in vicinity of symmetrical fuselage at Mach numbers 1.8 and 2.0
| Author: | Wise, George A |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E52E13 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59223/ |