Год выпуска: 2012 Автор: Ahmed Kadhim Hussein Издательство: LAP Lambert Academic Publishing Страниц: 196 ISBN: 9783848444472
Описание
This book deals with the aerodynamics of supersonic flying bodies where the shock waves are captured accurately , also the results explain the mesh generation over a two and three-dimensional missile and Mach number contours, temperature contours, pressure contours, density contours and internal energy contours for the selected range of Mach number which is tested for various missiles shapes.In recent years, a great attention is directed toward the simulation of flows around the missiles, since this simulation is the corner stone of the missiles design. Basically, the missile, is described as a weapon or object capable of being thrown or projected so as to strike a distant object. One distinction between a missile and an airplane is that, unlike an airplane, a missile is usually expendable in accomplishment of its mission.
