Aerodynamic calculation of the external flow around the front of the aircraft fuselage

A. L. Kalinova

Ulyanovsk State University, Ulyanovsk, Russia

Abstract: The article presents an aerodynamic calculation of the front part of the aircraft fuselage using Ansys software. The purpose of the calculation is to determine the effect of the air pressure discharged by the Environmental Control System of the aircraft for the perception of pressure by multifunctional air pressure measurement unit and a static pressure receiver (PSD).

Keywords: aerodynamic calculation, Environmental Control System, static pressure receiver, multifunctional air pressure measurement unit, flight speed, flight altitude.

UDC: 51-74

Received: 25.04.2019