The two-dimensional laminar boundary layer at hypersonic speeds
| dc.contributor.author | Nonweiler, T. | |
| dc.date.accessioned | 2012-09-11T09:50:17Z | |
| dc.date.available | 2012-09-11T09:50:17Z | |
| dc.date.issued | 1953-01 | |
| dc.description.abstract | A numerical solution is found for the equations governing the motion of a two-dimensional laminar boundary layer, in the absence of a pressure gradient, which would be valid if the flight Mach number is very high (i.e. M2>>1). The effects of surface slip, and the finite thickness of the boundary layer are shown to be negligible if the Reynolds Number (R) exceeds about 105, and are neglected. Continues … | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/7558 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics, Cranfield | en_UK |
| dc.relation.ispartofseries | College Reports | en_UK |
| dc.relation.ispartofseries | 67 | en_UK |
| dc.title | The two-dimensional laminar boundary layer at hypersonic speeds | en_UK |
| dc.type | Report | en_UK |