Aerodynamika těles při velmi vysokých hodnotách Machova čísla
Aerodynamics of Bodies at Very High Mach Numbers
| dc.contributor.advisor | Schmirler Michal | |
| dc.contributor.author | HyoungJu Lee | |
| dc.date.accessioned | 2023-08-23T22:51:42Z | |
| dc.date.available | 2023-08-23T22:51:42Z | |
| dc.date.issued | 2023-08-23 | |
| dc.identifier | KOS-1186952996005 | |
| dc.identifier.uri | http://hdl.handle.net/10467/111088 | |
| dc.description.abstract | This thesis work attempts to reproduce the NASA experiment regarding the aerodynamics of bodies at high Mach numbers 11.5, 19.5, and 34, using CFD simulation on Ansys Fluent software and compare the results to evaluate the accuracy of the simulation. Theoretical frameworks of hypersonic flow regime are presented with basic equations and principles, as well as appropriate CFD methods and conditions are going to be selected according to the body that was used in NASA experiment. | cze |
| dc.description.abstract | This thesis work attempts to reproduce the NASA experiment regarding the aerodynamics of bodies at high Mach numbers 11.5, 19.5, and 34, using CFD simulation on Ansys Fluent software and compare the results to evaluate the accuracy of the simulation. Theoretical frameworks of hypersonic flow regime are presented with basic equations and principles, as well as appropriate CFD methods and conditions are going to be selected according to the body that was used in NASA experiment. | eng |
| dc.publisher | České vysoké učení technické v Praze. Vypočetní a informační centrum. | cze |
| dc.publisher | Czech Technical University in Prague. Computing and Information Centre. | eng |
| dc.rights | A university thesis is a work protected by the Copyright Act. Extracts, copies and transcripts of the thesis are allowed for personal use only and at one?s own expense. The use of thesis should be in compliance with the Copyright Act http://www.mkcr.cz/assets/autorske-pravo/01-3982006.pdf and the citation ethics http://knihovny.cvut.cz/vychova/vskp.html | eng |
| dc.rights | Vysokoškolská závěrečná práce je dílo chráněné autorským zákonem. Je možné pořizovat z něj na své náklady a pro svoji osobní potřebu výpisy, opisy a rozmnoženiny. Jeho využití musí být v souladu s autorským zákonem http://www.mkcr.cz/assets/autorske-pravo/01-3982006.pdf a citační etikou http://knihovny.cvut.cz/vychova/vskp.html | cze |
| dc.subject | Hypersonic | cze |
| dc.subject | Mach number | cze |
| dc.subject | Boundary layers | cze |
| dc.subject | Ansys Fluent | cze |
| dc.subject | CFD | cze |
| dc.subject | Hypersonic | eng |
| dc.subject | Mach number | eng |
| dc.subject | Boundary layers | eng |
| dc.subject | Ansys Fluent | eng |
| dc.subject | CFD | eng |
| dc.title | Aerodynamika těles při velmi vysokých hodnotách Machova čísla | cze |
| dc.title | Aerodynamics of Bodies at Very High Mach Numbers | eng |
| dc.type | bakalářská práce | cze |
| dc.type | bachelor thesis | eng |
| dc.contributor.referee | Hyhlík Tomáš | |
| theses.degree.grantor | ústav mechaniky tekutin a termodynamiky | cze |
| theses.degree.programme | Teoretický základ strojního inženýrství | cze |
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Bakalářské práce - 12112 [118]