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Interaction theory of hypersonic laminar near-wake flow behind an adiabatic circular cylinder
| Content Provider | Semantic Scholar |
|---|---|
| Author | Hinman, W. Schuyler Johansen, Craig T. |
| Copyright Year | 2016 |
| Abstract | The separation and shock wave formation on the aft-body of a hypersonic adiabatic circular cylinder were studied numerically using the open source software OpenFOAM. The simulations of laminar flow were performed over a range of Reynolds numbers ($8\times 10^3 < Re < 8\times 10^4$8×103 |
| Starting Page | 717 |
| Ending Page | 727 |
| Page Count | 11 |
| File Format | PDF HTM / HTML |
| DOI | 10.1007/s00193-015-0615-y |
| Volume Number | 26 |
| Alternate Webpage(s) | http://tarjomefa.com/wp-content/uploads/2017/05/6635-English-TarjomeFa.pdf |
| Alternate Webpage(s) | https://doi.org/10.1007/s00193-015-0615-y |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |