Aerodynamics of Bodies at Very High Mach Numbers

dc.contributor.advisor Schmirler, Michal
dc.contributor.author Lee, HyoungJu
dc.contributor.referee Hyhlík, Tomáš
dc.date.accessioned 2023-08-23T22:51:42Z
dc.date.available 2023-08-23T22:51:42Z
dc.date.issued 2023-08-23
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. cs
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. en
dc.identifier KOS-1186952996005
dc.identifier.uri http://hdl.handle.net/10467/111088
dc.publisher České vysoké učení technické v Praze cs
dc.publisher Czech Technical University in Prague en
dc.rights A university thesis is a work protected by the Copyright Act of the Czech Republic. 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. en
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 v platném znění. cs
dc.subject Hypersonic cs
dc.subject Mach number cs
dc.subject Boundary layers cs
dc.subject Ansys Fluent cs
dc.subject CFD cs
dc.subject Hypersonic en
dc.subject Mach number en
dc.subject Boundary layers en
dc.subject Ansys Fluent en
dc.subject CFD en
dc.title Aerodynamika těles při velmi vysokých hodnotách Machova čísla cs
dc.title Aerodynamics of Bodies at Very High Mach Numbers en
dc.type bachelor thesis en
dspace.entity.type Publication
relation.isAdvisorOfPublication d453effd-1c32-4f06-8c88-c9678693a612
relation.isAdvisorOfPublication.latestForDiscovery d453effd-1c32-4f06-8c88-c9678693a612
relation.isAuthorOfPublication 585efee7-8240-42d9-8847-61b18e7b1a71
relation.isAuthorOfPublication.latestForDiscovery 585efee7-8240-42d9-8847-61b18e7b1a71
relation.isRefereeOfPublication b965ef5f-bd82-4bb6-b16a-3b873cb4ce38
relation.isRefereeOfPublication.latestForDiscovery b965ef5f-bd82-4bb6-b16a-3b873cb4ce38
theses.degree.grantor ústav mechaniky tekutin a termodynamiky cs
theses.degree.programme Teoretický základ strojního inženýrství cs

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