Computational study of a supersonic nose cone

Díaz Moncunill, Jordi

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Díaz Moncunill, Jordi

Author's e-mailjordi.diaz.moncunill

gmail.com

Tutor / directorCastilla López, Roberto

Document typeBachelor thesis

Date2018-06-10

Rights accessOpen Access

Except where otherwise noted, content on this work is licensed under a Creative Commons license : Attribution-NonCommercial-NoDerivs 3.0 Spain

Abstract

Generate the mesh Simulate the flow with the OpenFOAM supersonic flow solverData interpretationStudy of sensibility over the length

Description

The main objective is to obtain the temperature field and drag force around a nose cone of a supersonic rocket by means of Computational Fluid Dynamics.The secondary objectives are to learn techniques of CFD with Open Source code, and to apply these techniques to the improvement of actual supersonic roquets

SubjectsRockets (Aeronautics), Fluid dynamics (Space environment)), Coets (Aeronàutica), Dinàmica de fluids (Medi espacial)

DegreeGRAU EN ENGINYERIA EN VEHICLES AEROESPACIALS (Pla 2010)

URIhttp://hdl.handle.net/2117/328318

Collections

Escola Superior d'Enginyeries Industrial, Aeroespacial i Audiovisual de Terrassa - Grau en Enginyeria en Vehicles Aeroespacials (Pla 2010) [440]

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REPORT_556.pdf	3,067Mb	PDF	View/Open
ANNEX_381.pdf	368,7Kb	PDF	View/Open
BUDGET_568.pdf	204,3Kb	PDF	View/Open

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