Development of a flight simulator for conceptual aircraft design and sizing
Development of a flight simulator for conceptual aircraft design and sizing
This article describes the development of a flight simulator module within the ADEMAO aircraft design framework to investigate the effects of novel airframe and propulsion technologies on new generations of aircraft. Methods used to develop and integrate the fight simulator into the overall design framework are described. The simulator is validated based on existing data from the Convair CV-880M and is then used to analyze an example case of a conceptual medium-range aircraft with advanced airframe technologies designed in the Sustainable and Energy-Efficient Aviation research cluster at the Institute of Aircraft Design and Lightweight Structures at the Technische Universität Braunschweig. Results show the deficiencies of the medium-range aircraft in short-period pitch and Dutch roll performance, and recommendations for modifications to the conceptual medium-range aircraft are drafted.
31-61
Hon, Kai San
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Karpuk, Stanislav
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Yang, Daqing
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Elham, Ali
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Hon, Kai San
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Karpuk, Stanislav
583b7aff-008d-4d29-b697-01745a423095
Yang, Daqing
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Elham, Ali
676043c6-547a-4081-8521-1567885ad41a
Hon, Kai San, Karpuk, Stanislav, Yang, Daqing and Elham, Ali
(2022)
Development of a flight simulator for conceptual aircraft design and sizing.
Transactions on Aerospace Research, 2022 (2), .
(doi:10.2478/tar-2022-0009).
Abstract
This article describes the development of a flight simulator module within the ADEMAO aircraft design framework to investigate the effects of novel airframe and propulsion technologies on new generations of aircraft. Methods used to develop and integrate the fight simulator into the overall design framework are described. The simulator is validated based on existing data from the Convair CV-880M and is then used to analyze an example case of a conceptual medium-range aircraft with advanced airframe technologies designed in the Sustainable and Energy-Efficient Aviation research cluster at the Institute of Aircraft Design and Lightweight Structures at the Technische Universität Braunschweig. Results show the deficiencies of the medium-range aircraft in short-period pitch and Dutch roll performance, and recommendations for modifications to the conceptual medium-range aircraft are drafted.
Text
10.2478_tar-2022-0009
- Version of Record
More information
Accepted/In Press date: 1 April 2022
e-pub ahead of print date: 23 June 2022
Identifiers
Local EPrints ID: 483414
URI: http://eprints.soton.ac.uk/id/eprint/483414
ISSN: 2545-2835
PURE UUID: 705f0e6a-a42a-4ec7-abfb-3ec7fd2d3eb8
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Date deposited: 30 Oct 2023 17:47
Last modified: 17 Mar 2024 05:10
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Contributors
Author:
Kai San Hon
Author:
Stanislav Karpuk
Author:
Daqing Yang
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