Aerothermodynamics
Mostrando 1-8 de 8 artigos, teses e dissertações.
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1. A New Approach to Multidisciplinary Design Optimization of Solid Propulsion System Including Heat Transfer and Ablative Cooling
ABSTRACT: The optimum design of a solid propulsion system consists of optimization of various disciplines including structure, aerothermodynamics, heat transfer, and grain geometry. In this paper, an efficient model of every discipline has been developed, and a suitable framework is introduced for these hard-coupled disciplines. Hybrid optimization algorithm
J. Aerosp. Technol. Manag.. Publicado em: 2017-03
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2. Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic aerospace vehicle
Abstract 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 alternative, using a Supersonic Combustion Ramjet
J. Aerosp. Technol. Manag.. Publicado em: 2011-08
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3. Fragmentação por ação aerotermodinâmica e predição da área de impacto de um veículo espacial com injeção controlada da re-entrada / Aerothermodynamically-induced fragmentation and prediction of the area of impact of a space vehicle with controlled injection of the re-entry
Este trabalho consiste em estudar a fragmentação por ação aerotermodinâmica durante re-entrada de um veículo espacial, com estimativa da área de impacto dos fragmentos na superfície terrestre. Inicialmente, são realizadas manobras de decaimento orbital controlado através de transferências ótimas impulsivas. Tais impulsos são aplicados no sentido
Publicado em: 2009
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4. Aerothermodynamically-induced fragmentation and prediction of the area of impact of a space vehicle with controlled injection of the re-entry / Fragmentação por ação aerotermodinâmica e predição da área de impacto de um veículo espacial com injeção controlada da re-entrada
Este trabalho consiste em estudar a fragmentação por ação aerotermodinâmica durante re-entrada de um veículo espacial, com estimativa da área de impacto dos fragmentos na superfície terrestre. Inicialmente, são realizadas manobras de decaimento orbital controlado através de transferências ótimas impulsivas. Tais impulsos são aplicados no sentido
Publicado em: 2009
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5. Investigação Experimental da Adição de Energia por Laser em Escoamento Hipersônico de Baixa Densidade
The possibility of reducing the aerodynamic drag and heating of a hypersonic vehicle by addition energy to the air ahead of it is an attractive idea directed toward the hypersonic field. (Mach>5) and can be realized by laser induced plasma generation. In this context, this work presents original results in the experimental investigation of the energy addi
Publicado em: 2008
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6. Gas-surface interaction effect on round leading edge aerothermodynamics
Effects of incomplete surface accommodation in rarefied gas flow have been studied by using the Direct Simulation Monte Carlo (DSMC) method in conjunction with the Cercignani-Lampis-Lord gas surface interaction model. The DSMC calculations examine differences in predictions of aerodynamic forces and heat transfer between full and partial surface accommodatio
Brazilian Journal of Physics. Publicado em: 2007-06
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7. Simulation of blunt leading edge aerothermodynamics in rarefied hypersonic flow
The steady-state aerodynamic characteristics of a new family of blunted leading edges immersed in a high-speed rarefied air flow are examined by using a Direct Simulation Monte Carlo (DSMC) Method. A very detailed description of the flow properties has been presented separately at the vicinity of the nose and adjacent to the afterbody surface of the leading
Journal of the Brazilian Society of Mechanical Sciences and Engineering. Publicado em: 2007-06
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8. Direct Simulation Monte Carlo Method Applied to Aerothermodynamics
An axisymmetric supersonic flow of rarefied gas past a finite cylinder was calculated applying the direct simulation Monte Carlo method. The drag force, the coefficients of pressure, of skin friction, and of heat transfer, the fields of density, of temperature, and of velocity were calculated as function of the Reynolds number for a fixed Mach number. The va
Journal of the Brazilian Society of Mechanical Sciences. Publicado em: 2001