Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic aerospace vehicle

Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic aerospace vehicle

This paper presents a research in the development of the 14-X hypersonic airspace vehicle at Institute for Advanced Studies (IEAv) from Department of Science and Aerospace Technology (DCTA) of the Brazilian Air Force (FAB). The 14-X project objective is to develop a higher efficient satellite launch...

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Bibliographic Details
Main Authors: Tiago Cavalcanti Rolim, Paulo Gilberto de Paula Toro, Marco Antonio Sala Minucci, Antônio de Carlos de Oliveira, Roberto da Cunha Follador
Format: Article
Language:English
Published: Departamento de Ciência e Tecnologia Aeroespacial 2011-05-01
Series:Journal of Aerospace Technology and Management
Subjects:
Hypersonics
Hypersonic systems
Shock tunnel
Schlieren
Waverider
Online Access:http://www.jatm.com.br/papers/vol3_n2/JATMv3n2_p127-136_Experimental_results_of_a_mach_10_conical-flow_derived_waverider_to_14-X_hypersonic_airspace_vehicle.pdf

Internet

http://www.jatm.com.br/papers/vol3_n2/JATMv3n2_p127-136_Experimental_results_of_a_mach_10_conical-flow_derived_waverider_to_14-X_hypersonic_airspace_vehicle.pdf

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