dc.contributor.author |
I. McGregor |
en_US |
dc.date.accessioned |
2014-10-21T15:50:50Z |
|
dc.date.available |
2014-10-21T15:50:50Z |
|
dc.date.issued |
1972 |
en_US |
dc.identifier.other |
ARC/R&M-3728 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3005 |
|
dc.description.abstract |
Some comprehensive calculations of the flow conditions resulting from the intersection of a weak shock wave with a strong shock are presented and discussed, for a range of upstream Mach numbers between 1.4 and 2.8. Such flows are of interest in connection with the sub-critical stability of air intakes, for example, and in the interaction of shock waves and boundary layers. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Some calculations of conditions at the intersection of a weak shock wave with a strong shock |
en_US |