An “Integration Index” for Determining the Degree of Subsystem Integration in Passenger and Transport Aircraft Designs
30 déc. 2024
À propos de cet article
Catégorie d'article: Research Article
Publié en ligne: 30 déc. 2024
Pages: 27 - 44
Reçu: 09 déc. 2023
Accepté: 10 oct. 2024
DOI: https://doi.org/10.2478/tar-2024-0021
Mots clés
© 2024 Vasyl Loginov et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
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Fig. 4.

Ranges of variance in the values of the integration index_
Number of aircraft under study | Number and type of engine | |||
---|---|---|---|---|
6 | 4 turbojets | 0.4…0.7 | 4…11 | 7.5…12.8 |
9 | 2 turbofan | 3.4…6.7 | 12…17 | 8…25 |
5 | 2 turbofan + 1 turbojet | 2.1…3.0 | 13…17 | 10.8…30 |
10 | 4 turbofan | 1.1…2.0 | 14…22 | 12…40 |