| dc.creator |
Nonweiler, T. |
|
| dc.date |
2012-09-11T09:50:17Z |
|
| dc.date |
2012-09-11T09:50:17Z |
|
| dc.date |
1953-01 |
|
| dc.date.accessioned |
2022-05-09T10:17:19Z |
|
| dc.date.available |
2022-05-09T10:17:19Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7558 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4741 |
|
| dc.description |
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 … |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield |
|
| dc.relation |
College Reports |
|
| dc.relation |
67 |
|
| dc.title |
The two-dimensional laminar boundary layer at hypersonic speeds |
|
| dc.type |
Report |
|