Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel

Bibliographic Details
Main Author: IVAN FELIPE RODRIGUEZ BARON
Publication Date: 2014
Format: Master thesis
Source: Portal de Dados Abertos da CAPES
Download full: https://sucupira.capes.gov.br/sucupira/public/consultas/coleta/trabalhoConclusao/viewTrabalhoConclusao.jsf?popup=true&id_trabalho=1959633
id BRCRIS_5016ff37b83868498afc1e9d7019fd0b
network_acronym_str CAPES
network_name_str Portal de Dados Abertos da CAPES
dc.title.pt-BR.fl_str_mv Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
title Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
spellingShingle Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
aerospace vehicle.
IVAN FELIPE RODRIGUEZ BARON
title_short Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
title_full Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
title_fullStr Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
title_full_unstemmed Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
title_sort Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel
topic aerospace vehicle.
publishDate 2014
format masterThesis
url https://sucupira.capes.gov.br/sucupira/public/consultas/coleta/trabalhoConclusao/viewTrabalhoConclusao.jsf?popup=true&id_trabalho=1959633
author_role author
author IVAN FELIPE RODRIGUEZ BARON
author_facet IVAN FELIPE RODRIGUEZ BARON
dc.contributor.authorLattes.fl_str_mv http://lattes.cnpq.br/2356388448205325
dc.publisher.none.fl_str_mv INSTITUTO TECNOLÓGICO DE AERONÁUTICA
publisher.none.fl_str_mv INSTITUTO TECNOLÓGICO DE AERONÁUTICA
instname_str INSTITUTO TECNOLÓGICO DE AERONÁUTICA
dc.publisher.program.fl_str_mv Ciências e Tecnologias Espaciais
dc.description.course.none.fl_txt_mv Ciências e Tecnologias Espaciais
reponame_str Portal de Dados Abertos da CAPES
collection Portal de Dados Abertos da CAPES
spelling CAPESPortal de Dados Abertos da CAPESExperimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock TunnelExperimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock TunnelExperimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock TunnelExperimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock TunnelExperimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock TunnelExperimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock TunnelExperimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnelaerospace vehicle.2014masterThesishttps://sucupira.capes.gov.br/sucupira/public/consultas/coleta/trabalhoConclusao/viewTrabalhoConclusao.jsf?popup=true&id_trabalho=1959633authorIVAN FELIPE RODRIGUEZ BARONhttp://lattes.cnpq.br/2356388448205325INSTITUTO TECNOLÓGICO DE AERONÁUTICAINSTITUTO TECNOLÓGICO DE AERONÁUTICAINSTITUTO TECNOLÓGICO DE AERONÁUTICACiências e Tecnologias EspaciaisCiências e Tecnologias EspaciaisPortal de Dados Abertos da CAPESPortal de Dados Abertos da CAPES
identifier_str_mv BARON, IVAN FELIPE RODRIGUEZ. Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel. 2014. Tese.
dc.identifier.citation.fl_str_mv BARON, IVAN FELIPE RODRIGUEZ. Experimental Investigation of the Scramjet Demonstrator 14-X B at Mach Number 6 to 12 in the Hypersonic Shock Tunnel. 2014. Tese.
_version_ 1741888801995751424

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