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Numerical solution of the hypersonic viscous-shock-layer equations for laminar, transitional, and turbulent flows of a perfect gas over blunt axially symmetric bodies
| Content Provider | Semantic Scholar |
|---|---|
| Author | Anderson, Ernest C. Moss, James N. |
| Copyright Year | 1975 |
| Abstract | The viscous-shock-layer equations applicable to hypersonic laminar, transitional, andturbulent flows of a perfect gas over two-dimensional plane or axially symmetric blunt bodiesare presented. The equations are solved by means of an implicit finite-difference scheme,and the results are compared with a turbulent-boundary-layer analysis. The agreementbetween the two solution procedures is satisfactory for the region of flow where streamlineswallowing effects are negligible. For the downstream regions, where streamline swallowingeffects are present, the expected differences in the two solution procedures are evident. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750008700.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |