METHOD OF SUBSTANTIATION OF THE SCHEME AND SELECTION OF PARAMETERS OF THE POWER PLANT FOR AIRCRAFT FOR FLIGHT SPEED Mp = 0 ... 5

Ю. А. Улитенко, О. В. Кислов

Abstract


In this article, we briefly review the main aspects of the method of justifying the choice of the circuit and the parameters of the power plant of an aircraft with flight speeds from 0 to 5 Mach numbers in the early stages of design. The analysis of existing methods is carried out. The algorithm for performing operations for determining the optimum composition and parameters of the power plant, as well as the size of the aircraft depending on the mass of the payload, is stated and justified. Application of the obtained results will allow to shorten the terms of creation of competitive engines for high-speed aircraft due to a purposeful search for their rational thermodynamic and constructive-geometric appearance.

Keywords


method, aircraft, unmanned aerial vehicle, power plant, payload, air-jet engine, thrust.

References


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DOI: https://doi.org/10.32620/aktt.2017.7.01