Nicolosi, Fabrizio and Corcione, Salvatore and Trifari, Vittorio and De Marco, Agostino (2021) Design and Optimization of a Large Turboprop Aircraft. Aerospace, 8 (5). p. 132. ISSN 2226-4310
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Abstract
This paper proposes a feasibility study concerning a large turboprop aircraft to be used as a lower environmental impact solution to current regional jets operated on short/medium hauls. An overview of this market scenario highlights that this segment is evenly shared between regional turboprop and jet aircraft. Although regional jets ensure a large operative flexibility, they are usually not optimized for short missions with a negative effect on block fuel and environmental impact. Conversely, turboprops represent a greener solution but with reduced passenger capacity and speed. Those aspects highlight a slot for a new turboprop platform coupling higher seat capacity, cruise speed and design range with a reduced fuel consumption. This platform should operate on those ranges where neither jet aircraft nor existing turboprops are optimized. This work compares three different solutions: a high-wing layout with under-wing engines installation and both two- and three-lifting-surface configurations with low-wing and tail tips-mounted engines. For each concept, a multi-disciplinary optimization was performed targeting the minimum block fuel on a 1600 NM mission. Optimum solutions were compared with both a regional jet such as the Airbus A220-300 operated on 1600 NM and with a jet aircraft specifically designed for this range.
Item Type: | Article |
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Subjects: | Institute Archives > Medical Science |
Depositing User: | Managing Editor |
Date Deposited: | 07 Apr 2023 04:41 |
Last Modified: | 11 Jan 2024 03:54 |
URI: | http://eprint.subtopublish.com/id/eprint/1056 |