Follow
Augusto Fontan Moura
Augusto Fontan Moura
Applications Engineer, DCS Computing GmbH
Verified email at dcs-computing.com
Title
Cited by
Cited by
Year
Characterization of supersonic turbulent combustion in a mach-10 scramjet combustor
AF Moura, N Gibbons, V Wheatley, T McIntyre, I Jahn
AIAA Journal 58 (5), 2180-2196, 2020
162020
A numerical investigation of scramjet engine air intakes for the 14-x hypersonic vehicle
AF Moura, MAP Rosa
11th World Congress on Computational Mechanics, 20-25, 2014
92014
Effects of oxygen enrichment on supersonic combustion in a Mach 10 scramjet
AF Moura, N Gibbons, V Wheatley, I Jahn
AIAA Journal 59 (11), 4556-4568, 2021
72021
Thermofluidic compression effects to achieve combustion in a low-compression scramjet engine
AF Moura, V Wheatley, I Jahn
Shock Waves 28, 863-875, 2018
72018
Investigation of supersonic turbulent combustion in a Mach 10 scramjet engine
AF Moura
Doctor of Philosophy, The Univ. of Queensland, Brisbane, Australia, 2019
52019
On the development of a Mach 10 scramjet engine for investigation of supersonic combustion regimes
AF Moura, V Wheatley, TJ McIntyre, I Jahn
Proceedings of the 20th Australasian Fluid Mechanics Conference, AFMC 2016, 2016
42016
A Computer Program for Calculating Normal and Oblique Shock Waves for Airflows in Chemical and Thermodynamic Equilibrium
AF Moura, MAP Rosa
22nd International Congress of Mechanical Engineering, 2323-2333, 2013
42013
A NUMERICAL ANALYSIS OF BOUNDARY-LAYER/SHOCK WAVE INTERACTIONS IN THE COMPRESSION RAMPS OF SCRAMJET INTAKES
AF Moura, MAP Rosa
23rd ABCM International Congress of Mechanical Engineering, 2015
32015
A computational study of the airflow at the intake region of scramjet engines
AF Moura
32014
Comparing open-source DEM frameworks for simulations of common bulk processes
M Dosta, D Andre, V Angelidakis, RA Caulk, MA Celigueta, B Chareyre, ...
Computer Physics Communications 296, 109066, 2024
2024
Correction: Characterization of Supersonic Turbulent Combustion in a Mach-10 Scramjet Combustor
AF Moura, N Gibbons, V Wheatley, T McIntyre, I Jahn
AIAA Journal 59 (4), 1-1, 2021
2021
Correction to: Thermofluidic compression effects to achieve combustion in a low-compression scramjet engine
AF Moura, V Wheatley, I Jahn
Shock Waves 29, 901-901, 2019
2019
Análise da troca de calor em sistemas de injeção de termoplásticos–um estudo de caso: polipropileno
AF Moura
Universidade Estadual Paulista (Unesp), 2011
2011
Effects of oxygen enrichment on supersonic combustion in a Mach 10 scramjet combustor
AF Moura, N Gibbons, V Wheatley, I Jahn
The system can't perform the operation now. Try again later.
Articles 1–14