Aerodynamics of Bodies at Very High Mach Numbers

Aerodynamika těles při velmi vysokých hodnotách Machova čísla

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České vysoké učení technické v Praze
Czech Technical University in Prague

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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.

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.

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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.

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.

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