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Fluid–structure interaction study of the start-up of a rocket engine nozzle.
(Pergamon-elsevier Science Ltd, 2010-04)
The aim of this paper is to analyze the aeroelastic processes developed during the starting phase of a rocket engine via a coupling fluid/structure code. This analysis gives a better understanding of the behavior of the ...
Fluid-structure interaction study of the start-up of a rocket engine nozzle
(Elsevier, 2010-08)
The aim of this paper is to analyze the aeroelastic processes developed during the starting phase of a rocket engine via a coupling fluid/structure code. This analysis gives a better understanding of the behavior of the ...
Adaptive Simulation of the Internal Flow in a Rocket Nozzle
(Planta Piloto de Ingeniería Química, 2014-07)
This work is a first step in the understanding of the interaction process between internal shock waves and the flow transition inside of a rocket nozzle that develops during the engine start-up phase or when the nozzle is ...
Processing and characterization of ablative composites used in rocket motors
(Sage Publications Ltd, 2014-08-01)
The main objective of this research work was to obtain two formulations of ablative composites. These composites are also known as ablative structural composites, for applications in atmospherically severe conditions ...
Estudo numérico de um bocal convergente-divergente em motor-foguete
(Universidade Tecnológica Federal do ParanáCornelio ProcopioBrasilEngenharia MecânicaUTFPR, 2018-05-25)
Convergent-Divergent nozzles are essential parts in rocket propulsion systems, a lot has been developed over the study of these nozzles, however, those studies are focused on large systems. The goal of this study was the ...
Processing and characterization of ablative composites used in rocket motors
(Sage Publications Ltd, 2015)
Processing and characterization of ablative composites used in rocket motors
(Sage Publications Ltd, 2015)
Concepção de um veículo lançador de microssatélite baseado em foguetes de sondagem desenvolvidos no Brasil
(Universidade Federal de Santa MariaBrasilUFSMCentro de Tecnologia, 2020-09-28)
The present work presents a proposal that involves reverse engineering of the current solid
rocket engines developed by the Aeronautics and Space Institute (IAE), for the design of a
Microsatellite Launch Vehicle (VLM). ...