URI | http://purl.tuc.gr/dl/dias/29A03A5F-0BA4-45A1-8BE4-D3B8BBC027E7 | - |
Αναγνωριστικό | https://www.scopus.com/inward/record.uri?eid=2-s2.0-85143252737&partnerID=40&md5=4b2cee97bcb14b0889140af759409a7b | - |
Γλώσσα | en | - |
Τίτλος | Computation of hypersonic flow around an isolated roughness element using kinetic theory | en |
Δημιουργός | Klothakis Angelos | en |
Δημιουργός | Κλωθακης Αγγελος | el |
Δημιουργός | Dylewicz Kamil | en |
Δημιουργός | Theofilis, Vassilis | en |
Δημιουργός | Sawant Saurabh S. | en |
Δημιουργός | Levin Deborah A. | en |
Εκδότης | Technion Israel Institute of Technology | en |
Περίληψη | 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 |
Τύπος | Πλήρης Δημοσίευση σε Συνέδριο | el |
Τύπος | Conference Full Paper | en |
Άδεια Χρήσης | http://creativecommons.org/licenses/by/4.0/ | en |
Ημερομηνία | 2024-12-20 | - |
Ημερομηνία Δημοσίευσης | 2022 | - |
Θεματική Κατηγορία | Aerospace engineering | en |
Θεματική Κατηγορία | Computation theory | en |
Θεματική Κατηγορία | Direct Simulation Monte Carlo methods | en |
Βιβλιογραφική Αναφορά | 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 |