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Development of a flight simulator for conceptual aircraft design and sizing

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.
2545-2835
31-61
Hon, Kai San
5cbd8ed9-b893-4b99-87f5-a7f1ec2a8d24
Karpuk, Stanislav
583b7aff-008d-4d29-b697-01745a423095
Yang, Daqing
2e7bbd2b-b9f3-44e4-a31e-66ccb7d0466f
Elham, Ali
676043c6-547a-4081-8521-1567885ad41a
Hon, Kai San
5cbd8ed9-b893-4b99-87f5-a7f1ec2a8d24
Karpuk, Stanislav
583b7aff-008d-4d29-b697-01745a423095
Yang, Daqing
2e7bbd2b-b9f3-44e4-a31e-66ccb7d0466f
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), 31-61. (doi:10.2478/tar-2022-0009).

Record type: Article

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.

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10.2478_tar-2022-0009 - Version of Record
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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
Author: Ali Elham

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