COMPUTER MODEL OF AN AIRCRAFT TURBULENT FLOW OVER AND CALCULATION OF IT’S AERODYNAMIC CHARACTERISTICS

Abstract

The original semiempirical model of turbulent flow of air in an interface of an aircraft surface is described in this work. Based on this model the computer system allowing to simulate aerodynamic processes around an aircraft and to calculate it’s aerodynamic characteristics was developed. These characteristics are used by aircraft designers for an assessment of quality and properties of an aircraft.