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

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 cha...

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Bibliographic Details
Main Authors: Yu. V. Yatskevich, Yu. V. Kozedub
Format: Article
Language:English
Published: Belarusian National Technical University 2015-08-01
Series:Sistemnyj Analiz i Prikladnaâ Informatika
Online Access:https://sapi.bntu.by/jour/article/view/46