Methodical and algorithmic aspects of mathematical modeling of a screw aircraft power plant
- Authors: Zinenkov Y.V.1
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Affiliations:
- Military Educational and Scientific Center of the Air Force Academy named after Professor N.E. Zhukovsky and Yu.A. Gagarin
- Issue: Vol 23, No 3 (2024)
- Pages: 82-93
- Section: MECHANICAL ENGINEERING
- URL: https://journals.rcsi.science/2542-0453/article/view/311479
- DOI: https://doi.org/10.18287/2541-7533-2024-23-3-82-93
- ID: 311479
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Abstract
The article describes the solution of a scientific problem that consists in expanding the functionality of the program “Calculation of the traction-economic and mass-specific characteristics of the power plant and aircraft motion parameters” through the introduction of additional algorithms and mathematical models for calculating the altitude-speed characteristics of screw aircraft power installations. At the same time, an internal calculation of the aircraft propeller thrust is used according to experimental aerodynamic coefficients, which makes it possible to increase the efficiency and reliability of complex theoretical studies of power plants of various types as part of aircraft at the stage of external design. A description is given of the developed algorithms: an algorithm for converting power on the output shaft of a gas turbine engine into thrust of an aircraft power plant; a mathematical model of a propeller that provides calculation of its thrust from experimental aerodynamic coefficients; an algorithm for determining the thrust of the power plant, taking into account the compressibility of the air and the interaction of the propeller and the elements of the airframe of the aircraft. Some features of the mathematical modeling of an aircraft propeller are revealed, in particular, the principle of propeller control by influencing the blade angle and rotational speed depending on the aircraft flight speed and a method for constructing the field of aerodynamic characteristics of an aircraft propeller in a wide range of blade angle and speed coefficient. In conclusion, the results of verification of the modified program are presented with an analysis of the obtained altitude-speed characteristics.
About the authors
Yu. V. Zinenkov
Military Educational and Scientific Center of the Air Force Academy named after Professor N.E. Zhukovsky and Yu.A. Gagarin
Author for correspondence.
Email: Zinenkovy@mail.ru
Candidate of Science (Engineering), Doctoral Student
Russian FederationReferences
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