doi ISSN Leading-to-trailing edge theoretical design of a generic scramjet (AIP Advances)

doi ISSN Optimization of scramjet inlet based on temperature and Mach number of supersonic combustion (AEROSPACE SCIENCE AND TECHNOLOGY)

doi ISSN Preliminary Study of Launch and Orbit of a CubeSat Using a Modified VSB-30 Launcher Vehicle (JOURNAL OF AEROSPACE TECHNOLOGY AND MANAGEMENT (ONLINE))

doi ISSN Experimental Study of Single Expansion Ramp Nozzle Performance Using Pitot Pressure and Static Pressure Measurements (International Journal of Aerospace Engineering)

doi ISSN Experimental Investigation of Brazilian 14-X B Hypersonic Scramjet Aerospace Vehicle (International Journal of Aerospace Engineering)

doi ISSN Ground experimentation with 3D printed scramjet inlet models at hypervelocities (Aerospace Science and Technology (Imprimé))

doi DEVELOPMENT AND COMPARISON OF PLANAR AND CONICAL SCRAMJET VEHICLE INLET (26th International Congress of Mechanical Engineering)

doi DEVELOPMENT OF ROCKET MOTOR TRANSIENT THERMAL ANALYSIS SOFTWARE (26th International Congress of Mechanical Engineering)

doi MODELING, IMPLEMENTATION AND APPLICATION OF A TOOL FOR PRELIMINARY HYPERSONIC AIRBREATHING VEHICLE DESIGN (26th International Congress of Mechanical Engineering)

doi SCRAMJET DESIGN FOR ATMOSPHERIC FLIGHT FROM 23 KM TO 30 KM (26th International Congress of Mechanical Engineering)

doi SYSTEM ENGINEERING APPLIED TO HIGH POWER ROCKET DEVELOPMENT (26th International Congress of Mechanical Engineering)

Cubesat Launch for Mission on Mars Using a Small Dedicated Launcher and Electric Propulsion. (5th IAA Conference on University Satellite Missions and Cubesat Workshop)

doi MODELAGEM DE UM MOTOR SCRAMJET AXISSIMÉTRICO (2º Congresso Aeroespacial Brasileiro)

doi PROJETO AEROTERMODINÂMICO DO SISTEMA DE ADMISSÃO DE UM MOTOR SCRAMJET (2º Congresso Aeroespacial Brasileiro)

A New Approach to Optimize the Scramjet Inlet Design Applying the Total Pressure Recovery (17th Brazilian Congress of Thermal Sciences and Engineering)

Aerodynamic Characterization of a Hooded Fairing Accommodating Winged Payloads (International Conference on High-Speed Vehicle Science and Technology)

Chemical Reactions Model Applied to Supersonic Combustion (17th Brazilian Congress of Thermal Sciences and Engineering)

Design and Analysis of a Generic Scramjet Air Inlet (17th Brazilian Congress of Thermal Sciences and Engineering)

Design of an Academic Scramjet for Atmospheric Captive Flight at Mach Number 4.18 Coupled to a Rocket FTI (17th Brazilian Congress of Thermal Sciences and Engineering)

Design of the Generic Scramjet Combustion Chamber (17th Brazilian Congress of Thermal Sciences and Engineering)

doi High temperature effects in conical nozzle flow (22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference)

Preliminary Design of a Hooded Fairing Accommodating Winged Payloads (International Conference on High-Speed Vehicle Science and Technology)

doi Preliminary Studies on Hypersonic Flows Over 3D Printed Models (22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference)

Projeto da Seção de Compressão do Scramjet Acadêmico da UFRN para Voo Atmosférico Acoplado ao Foguete de Treinamento (CONEM 2018)

doi 3D Prototyping Model Design for Experimental Investigation in Hypersonic Shock Tunnel (21st AIAA International Space Planes and Hypersonics Technologies Conference)

doi Experimental Analysis of 14-X B Hypersonic Aerospace Vehicle Compression System (21st AIAA International Space Planes and Hypersonics Technologies Conference)

Numerical Study of Flow Characteristics of the 14-X B Hypersonic Aerospace Vehicle Inlet with Blunted Leading Edge (7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS))

Concepção de Modelo em Prototipagem 3D para Investigação Experimental em Túnel de Choque Hipersônico (IX Congresso Nacional de Engenharia Mecânica)

Estudo Teórico-Analítico do Veículo Hipersônico Aeroespacial Brasileiro 14-X B (IX Congresso Nacional de Engenharia Mecânica)

Experimental Investigation of the Brazilian 14-X B Hypersonic Scramjet Aerospace Vehicle (IX Congresso Nacional de Engenharia Mecânica)

Investigação Experimental de um Motor Scramjet de Admissão Interna (IX Congresso Nacional de Engenharia Mecânica)

Unsteady Flow Field in a Shock Tube: Solutions, CFD and Experiments (IX Congresso Nacional de Engenharia Mecânica)

Análise das Medidas de Controle do Perigo Aviário (6 Simpósio de Segurança de Voo)

Pesquisa Scramjet no IEAv (XVI Workshop Anual de Pesquisa e Desenvolvimento do IEAv)

Projeto 14-X S (XVI Workshop Anual de Pesquisa e Desenvolvimento do IEAv)

Projeto 14-X S (XV Workshop Anual de Pesquisa e Desenvolvimento do IEAv)

Projeto de Demonstradores Tecnológicos 'scramjet' no IEAv (XIV Workshop Anual de Pesquisa e Desenvolvimento do IEAv,)

Projeto de Demonstradores Tecnológicos scramjet no IEAv (V Fórum de Pesquisa e Inovação do CLBI)

Análisis del Efecto de Alta Temperatura en el Flujo de Tubo de Choque (4to Congreso Argentino de Ingeniería Aeronáutica)

Análisis Térmica del Vehículo Hipersonico Aeroespacial Brasilero 14-X en Numero de Mach 10 (4º Congresso Argentino de Ingeniería Aeronáutica)

Investigación Experimental del Vehículo Aeroespacial Brasilero 14-X B (4º Congresso Argentino de Ingeniería Aeronáutica)

Projeto Aerotermodinâmico de um Demonstrador Tecnológico Scramjet (Simpósio de Ciência, Tecnologia e Inovação do IEAv)

Investigação Experimental do Veículo Hipersônico Aeroespacial (Congresso Nacional das Engenharias da Mobilidade)

Computational fluid dynamics (CFD) for hypersonics flow

Numerical simulation applied to scramjet

3D Prototyping Model Design for Experimental Investigation in Hypersonic Shock Tunnel

Experimental Analysis of 14-X B Hypersonic Aerospace Vehicle Compression

Global Report - Brazil

Experimental Investigation of the Brazilian 14-X B Hypersonic Scramjet Aerospace Vehicle

Experimental Investigation of the Inlet of the VHA 14-X B at Mach Number 7

Análise das medidas de controle do perigo aviário

Investigação Experimental Do Veículo Hipersônico Aeroespacial 14-X B

Análise de Tendências das Medidas de Controle do Perigo Aviário para Redução de Risco de Acidentes Aeronáuticos

Controle do Perigo Aviário

Concepção de um Veículo Lançador de Microssatélite Baseado em Foguetes de Sondagem Desenvolvidos no Brasil

Modelagem e Implementação de Ferramenta para Projeto Preliminar de Motor Hipersônico Aspirado

Preliminary Design of a Ludwieg Tube as an Experimental Facility for a Laboratory of Compressible Flows at UFSM