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An “Integration Index” for Determining the Degree of Subsystem Integration in Passenger and Transport Aircraft Designs Cover

An “Integration Index” for Determining the Degree of Subsystem Integration in Passenger and Transport Aircraft Designs

By: Vasyl Loginov and  Oleg Anipko  
Open Access
|Dec 2024

Figures & Tables

Fig. 1.

Dependence of the integration index on the characteristics of the engine and aircraft (with 4 turbojets).
Dependence of the integration index on the characteristics of the engine and aircraft (with 4 turbojets).

Fig. 2.

Dependence of the integration index on the characteristics of the engine and aircraft (with 2 turbofan engines).
Dependence of the integration index on the characteristics of the engine and aircraft (with 2 turbofan engines).

Fig. 3.

Dependence of the integration index on the characteristics of the engine and aircraft (with 3 turbofan engines).
Dependence of the integration index on the characteristics of the engine and aircraft (with 3 turbofan engines).

Fig. 4.

Dependence of the integration index on the characteristics of the engine and aircraft (with 4 turbofan engines).
Dependence of the integration index on the characteristics of the engine and aircraft (with 4 turbofan engines).

Ranges of variance in the values of the integration index_

Number of aircraft under studyNumber and type of engineПintegrationKA/CSmidel, m2
64 turbojets0.4…0.74…117.5…12.8
92 turbofan3.4…6.712…178…25
52 turbofan + 1 turbojet2.1…3.013…1710.8…30
104 turbofan1.1…2.014…2212…40
Language: English
Page range: 27 - 44
Submitted on: Dec 9, 2023
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Accepted on: Oct 10, 2024
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Published on: Dec 30, 2024
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2024 Vasyl Loginov, Oleg Anipko, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.