ON THE QUESTION OF COMPARISON OF AERODYNAMIC PARAMETERS OF NUMERICAL AND INTEGRAL METHODS FOR CALCULATION OF A TURBULENT NONISOTHERMAL JET IN A CYLINDRICAL CHANNEL
The paper presents a comparison of aerodynamic performance of flow structure resulting from the interaction of non-isothermal turbulent jet and a cocurrent flow in a cylindrical channel, the numerical and integral methods. Regarded for their education at the wall of the zones of reverse currents, and without them. The basic laws studied jet streams. The paper discusses the main portion of the turbulent jet.