Experimental Investigation of Ionization Sensors Under Shock Tube Stagnation Conditions

Autor: Rafael Augusto Cintra, Tiago Cavalcanti Rolim, Bruno Coelho Lima

Publikováno v: Journal of Aerospace Technology and Management, Vol 9, Iss 2 (2017)

Recently, there has been a growing interest in studies concerning ionization sensors for aerospace applications, power generation, and fundamental research. In aerospace research, they have been used for studies of shock and detonation waves. Two key

Externí odkaz: https://doaj.org/article/c7ff622db4c249dd979305ef501279f0

Ground experimentation with 3D printed scramjet inlet models at hypervelocities

Autor: Victor Alves Barros Galvão, Jayme Rodrigues Teixeira Silva, Israel da Silveira Rêgo, Thiago Victor Cordeiro Marcos, G.P. Camilo, Antonio Carlos de Oliveira, Ronaldo de Lima Cardoso, D. Romanelli Pinto, Bruno Coelho Lima, Alexandra M. Santos, Álvaro Francisco Santos Pivetta, Paulo Toro, A.K. Carvalhal, Renan Guilherme Santos Vilela, Joao Felipe de Araujo Martos

Publikováno v: Aerospace Science and Technology. 55:307-313

3D printing technologies have gained acceptance by aerospace engineers as an alternative way for manufacturing models for experimentation in wind tunnels. This paper addresses ground experimentations with polymer-based 3D printed models of a single r

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::ab5bcd880c0cbf95534381eb4a7a2825
https://doi.org/10.1016/j.ast.2016.06.009

Preliminary Design of an Aerodynamic Protection for the scramjet Engine Inlet of the Brazilian Technological Demonstrator scramjet 14-X S

Autor: Ronaldo d. Cardoso, Israel d. Rêgo, Paulo Toro, Dercy Felix da Silva, Marco Antonio Sala Minucci, Bruno Coelho Lima, Felipe Jean da Costa, Gustavo Jean da Costa, David Romanelli Pinto, Antonio Carlos de Oliveira

Publikováno v: 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::592e80fd0cf469e07196c8d76802fceb
https://doi.org/10.2514/6.2018-5386

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

Autor: Sergio Nicholas Pachon Laiton, Joao Felipe de Araujo Martos, Paulo Toro, Felipe Jean da Costa, Bruno Coelho Lima, Israel da Silveira Rêgo

Publikováno v: International Journal of Aerospace Engineering, Vol 2017 (2017)

The Brazilian hypersonic scramjet aerospace vehicle 14-X B is a technological demonstrator of a hypersonic airbreathing propulsion system based on the supersonic combustion (scramjet) to be tested in flight into the Earth’s atmosphere at an altitud

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::00edbe60d66ec929d24b8e267e81f3a1
https://doaj.org/article/941cbeabfaa6424daa3806e7c4066919

EXPERIMENTAL INVESTIGATION OF IONIZATION SENSORS UNDER SHOCK TUBE STAGNATION CONDITIONS

Autor: Bruno Coelho Lima, Tiago Cavalcanti Rolim, Rafael Augusto Cintra

Publikováno v: Journal of Aerospace Technology and Management v.9 n.2 2017
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 9, Issue: 2, Pages: 218-224, Published: JUN 2017

Recently, there has been a growing interest in studies concerning ionization sensors for aerospace applications, power generation, and fundamental research. In aerospace research, they have been used for studies of shock and detonation waves. Two key

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7d42ad074ef5b71cccae3f0f67eb8eb1
https://doi.org/10.26678/abcm.encit2016.cit2016-0278