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Technical University of Crete
Technical University of Crete
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| URI | http://purl.tuc.gr/dl/dias/29A03A5F-0BA4-45A1-8BE4-D3B8BBC027E7 | - |
| Identifier | https://www.scopus.com/inward/record.uri?eid=2-s2.0-85143252737&partnerID=40&md5=4b2cee97bcb14b0889140af759409a7b | - |
| Language | en | - |
| Title | Computation of hypersonic flow around an isolated roughness element using kinetic theory | en |
| Creator | Klothakis Angelos | en |
| Creator | Κλωθακης Αγγελος | el |
| Creator | Dylewicz Kamil | en |
| Creator | Theofilis, Vassilis | en |
| Creator | Sawant Saurabh S. | en |
| Creator | Levin Deborah A. | en |
| Publisher | Technion Israel Institute of Technology | en |
| Content Summary | The effect of an isolated cylindrical roughness element embedded in a laminar boundary layer on a semi-infinite flat plate in rarefied Mach 6 flow is studied using Direct Simulation Monte Carlo methods. Steady state solutions are computed in the three-dimensional configuration, two-dimensional results are obtained on the symmetry plane cutting through the cylinder center and the topologically different structure of laminar separation ahead of and behind the roughness element is documented and briefly discussed. Linear BiGlobal instability analysis of the flow field downstream of the roughness element has revealed stable, traveling, symmetric global modes. | en |
| Type of Item | Πλήρης Δημοσίευση σε Συνέδριο | el |
| Type of Item | Conference Full Paper | en |
| License | http://creativecommons.org/licenses/by/4.0/ | en |
| Date of Item | 2024-12-20 | - |
| Date of Publication | 2022 | - |
| Subject | Aerospace engineering | en |
| Subject | Computation theory | en |
| Subject | Direct Simulation Monte Carlo methods | en |
| Bibliographic Citation | A. Klothakis, K. Dylewicz, V. Theofilis, S. S. Sawant and D. A. Levin, "Computation of hypersonic flow around an isolated roughness element using kinetic theory," in Proceedings of the 61st Israel Annual Conference on Aerospace Science (IACAS 2022), 2022. | en |
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