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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

Transactions on Aerospace Research
Volume 2024 (2024): Issue 4 (December 2024)
By:  and    
Open Access
|Dec 2024
Figures & tables

Figures & Tables

Fig. 1.

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).

Fig. 3.

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).

Table 1.

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
DOI: https://doi.org/10.2478/tar-2024-0021 | Journal eISSN: 2545-2835
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Language: English
Page range: 27 - 44
Submitted on: Dec 9, 2023
Accepted on: Oct 10, 2024
Published on: Dec 30, 2024
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Keywords:
complex method,
parametric appearance,
propulsion system,
airframe,
degree of rationality,
integration,
technical perfection
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other,
Geosciences,
Geosciences, other,
Materials sciences,
Materials sciences, other,
Physics,
Physics, other

© 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.

Volume 2024 (2024): Issue 4 (December 2024)
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