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Uchenyye zapiski UlGU. Seriya "Matematika i informatsionnyye tekhnologii", 2019, Issue 1, Pages 41–46
(Mi ulsu63)
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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.
Received: 25.04.2019
Citation:
A. L. Kalinova, “Aerodynamic calculation of the external flow around the front of the aircraft fuselage”, Uchenyye zapiski UlGU. Seriya “Matematika i informatsionnyye tekhnologii”, 2019, no. 1, 41–46
Linking options:
https://www.mathnet.ru/eng/ulsu63 https://www.mathnet.ru/eng/ulsu/y2019/i1/p41
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Abstract page: | 41 | Full-text PDF : | 45 | References: | 9 |
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