Effects of Cone Angle and Inlet Blade Angle on Mixed Inflow Turbine Performances

Autor:	Mohammed Kamel Hamidou, Mohammed Hamel, Mohammed Amine Chelabi
Rok vydání:	2017
Předmět:	Engineering drawing geography geography.geographical_feature_category Mechanical Engineering Bézier curve Inflow Mechanics Inlet Turbine Deflection (engineering) Turbomachinery Ligand cone angle Casing Mathematics
Zdroj:	Periodica Polytechnica Mechanical Engineering. 61:225
ISSN:	1587-379X 0324-6051
DOI:	10.3311/ppme.9890
Popis:	The development of the aerofoil-shaped turbomachine blades is of prime importance for achieving the appropriate deflection of a three dimensional flow through desired angles, to work at the same degree of incidence and thereby providing the required performances for the specific machine. The sensitivity of the rotor to incidence effects and tendency of the flow to separate from one or the other blade surface have given rise to considerations of the optimum incidence angle and cone angle for a mixed inflow turbine by a numerical investigation using the ANSYS-CFX code. In order to keep the rotor in the same casing some geometrical parameters have been hold constant and the Bezier polynomial is used to generate the new shape of the rotor blade when changing the cone angle magnitude.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::82889d963ad2d5389378f30e14d66f9d https://doi.org/10.3311/ppme.9890 Zobrazit plný text záznamu Plný text ve formátu PDF