Title :
Absolute cross-section of turbojet aviation engine calculation
Author :
Ryabokon, Evgen O.
Author_Institution :
Kharkiv Univ. of Air Forces, Kharkiv, Ukraine
Abstract :
The calculation method of three-dimensional model of turbojet aviation engine is offered, thus the form of turbine vanes with spiralling is described like parametric surface. The method allows make the calculation of absolute cross-section (ACS) of turbojet aviation engines with different geometrical parameters. The calculation results of ACS of aviation engine are presented.
Keywords :
blades; jet engines; turbines; engine absolute cross section calculation; geometrical parameters; turbine vanes; turbojet aviation engine; Blades; Engines; Mathematics; Optics; Turning; Absolute cross-section; Turbojet aviation engine;
Conference_Titel :
Modern Problems of Radio Engineering Telecommunications and Computer Science (TCSET), 2012 International Conference on
Conference_Location :
Lviv-Slavske
Print_ISBN :
978-1-4673-0283-8
