dc.creator |
Imbrioscia, Germán |
|
dc.creator |
Barceló, Luis Francisco |
|
dc.creator |
Vilar, Pablo |
|
dc.date.accessioned |
2018-10-08T12:54:19Z |
|
dc.date.available |
2018-10-08T12:54:19Z |
|
dc.date.issued |
2015 |
|
dc.identifier.uri |
http://hdl.handle.net/123456789/7537 |
|
dc.description.abstract |
Objetive: develop capabilities to calculate and
predict the behavior of a solid propellant rocket
nozzle under certain conditions, using numerical
methods. |
en |
dc.format.extent |
18 p. |
es |
dc.title |
Solid propellant rocket nozzle design and validation using Finite Difference Method and CFD technique |
es |
uade.subject.descriptor |
Modelado y Simulación |
es |
uade.subject.descriptor |
Mecánica Computacional |
es |
uade.proyecto.codigo |
A14T08 |
es |
uade.proyecto.nombre |
Fluidodinámica computacional – simulación y experimentos |
es |
uade.area |
Modelado y Simulación Computacional (transversal) |
es |
uade.linea |
Fluidodinámica Computacional |
es |
uade.proyecto.responsable |
Larreteguy, Axel |
|
uade.congreso |
1st Panamerican Congress on Computational Mechanics, 2015, Buenos Aires, Argentina. |
es |
uade.instituto |
Instituto de Tecnología |
es |