dc.contributor.author |
B. A. Woods |
en_US |
dc.date.accessioned |
2014-10-21T15:56:22Z |
|
dc.date.available |
2014-10-21T15:56:22Z |
|
dc.date.issued |
1963 |
en_US |
dc.identifier.other |
ARC/R&M-3413 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3997 |
|
dc.description.abstract |
The problem of calculating the supersonic flow past a circular cone at small incidence α is treated by the method of inner and outer expansions, on the assumption that it can be expressed as a perturbation (in powers of α) of the corresponding axially symmetric flow. Stone's first-order solution, and the first-order vortical-layer solution are connected as the first-order terms in the outer and inner expansions for the flow. It is shown that the logarithmic infinities which occurred in Stone's second-order solution are removed from the final (composite) solution for second-order terms by application of the generalized matching principle, and the second-order terms in the expansions of the inner solution are obtained. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
The supersonic flow past a circular cone at incidence |
en_US |