INVESTIGADORES
ELASKAR sergio Amado
congresos y reuniones científicas
Título:
Numerical simulation of Conic Object’s Dynamics Atmospheric Reentry
Autor/es:
CIMINO, ANDRÉS; SALDÍA, JUAN; SCHULZ, WALKIRIA; ELASKAR, SERGIO; FICO, NIDE
Lugar:
Sao Jose dos Campos
Reunión:
Congreso; 2009 Brazilian Symposium on Aerospace Engineering and Applications; 2009
Resumen:
&lt;!-- /* Style Definitions */ p.MsoNormal, li.MsoNormal, div.MsoNormal {mso-style-parent:""; margin:0cm; margin-bottom:.0001pt; mso-pagination:widow-orphan; font-size:10.0pt; font-family:"Times New Roman"; mso-fareast-font-family:"Times New Roman"; mso-ansi-language:EN-US; mso-fareast-language:PT-BR;} p.AuthorAddress, li.AuthorAddress, div.AuthorAddress {mso-style-name:"Author Address"; mso-style-parent:""; mso-style-next:Normal; margin-top:0cm; margin-right:0cm; margin-bottom:0cm; margin-left:2.85pt; margin-bottom:.0001pt; mso-pagination:widow-orphan lines-together; border:none; mso-border-left-alt:solid windowtext 2.25pt; padding:0cm; mso-padding-alt:0cm 0cm 0cm 4.0pt; font-size:9.0pt; mso-bidi-font-size:10.0pt; font-family:"Times New Roman"; mso-fareast-font-family:"Times New Roman"; mso-ansi-language:PT; mso-fareast-language:PT-BR; mso-no-proof:yes;} @page Section1 {size:612.0pt 792.0pt; margin:70.85pt 3.0cm 70.85pt 3.0cm; mso-header-margin:36.0pt; mso-footer-margin:36.0pt; mso-paper-source:0;} div.Section1 {page:Section1;} --&gt;  <!-- /* Style Definitions */ p.MsoNormal, li.MsoNormal, div.MsoNormal {mso-style-parent:""; margin:0cm; margin-bottom:.0001pt; mso-pagination:widow-orphan; font-size:12.0pt; font-family:"Times New Roman"; mso-fareast-font-family:"Times New Roman";} @page Section1 {size:595.3pt 841.9pt; margin:70.85pt 3.0cm 70.85pt 3.0cm; mso-header-margin:35.4pt; mso-footer-margin:35.4pt; mso-paper-source:0;} div.Section1 {page:Section1;} --> One of the key issues in a re-entry risk analysis is the calculation of the aerodynamic coefficients. This paper presents a methodology to obtain these coefficients and couple it to a code that computes re-entry trajectories considering six degrees of freedom. To evaluate the different flight conditions encountered during the natural re-entry of conical objects, the Euler Equations for gasdynamics flows are used. A new scheme TVD (Total Variation Diminishing) is incorporated to a finite volume unstructured cell-centred formulation, for application to three-dimensional Euler flows. Finally numerical results are obtained for a conical body at different attack angles and Mach. With these results, the calculation of the trajectories during atmospheric re-entry is completed.