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Design of the Propelling Nozzles for the Launchers and Satellites
Authors: R. Haoui
Abstract:The aim of this work is to determine the supersonic nozzle profiles used in propulsion, for the launchers or embarked with the satellites. This design has as a role firstly, to give a important propulsion, i.e. with uniform and parallel flow at exit, secondly to find a short length profiles without modification of the flow in the nozzle. The first elaborate program is used to determine the profile of divergent by using the characteristics method for an axisymmetric flow. The second program is conceived by using the finite volume method to determine and test the profile found connected to a convergent.
Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1061166Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 1441
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 R. Haoui, A. Gahmousse, D. Zeitoun, " Chemical and vibrational nonequilibrium flow in a hypersonic axisymmetric nozzle (Ecoulement hors d-équilibre chimique et vibrationnel dans une tuyère hypersonique axisymétrique), " International Journal of Thermal Sciences, article n┬░ 8 , volume 40, (2001), pp787-795.
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