Výsledky vyhledávání - "Cheung, Ronald C M"

Experimental Analysis of the Behaviour of Flared Folding Wingtips with Sideslip Angle

Autor: Healy, Fintan, Cheung, Ronald C M, Rezgui, Djamel, Cooper, Jonathan E

Publikováno v: Healy, F, Cheung, R C M, Rezgui, D & Cooper, J E 2022, ' Experimental Analysis of the Behaviour of Flared Folding Wingtips with Sideslip Angle ', Paper presented at 19th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2022, Madrid, Spain, 13/06/22-17/06/22 .

A concept of growing interest in recent years is that of the Flared Folding Wingtip (FFWT), which can be used in-flight to reduce airframe loading due to gust encounters and augment the handling qualities of an aircraft. The performance of an FFWT is

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______2642::5702c5ab1b3b7913754b1f0c0ce143e9
https://hdl.handle.net/1983/97c9811b-526a-47a4-aaff-0842b06380eb

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Nonlinear Stability Analysis and Experimental Exploration of Limit Cycle Oscillations with Flared Folding Wingtips

Autor: Healy, Fintan, Cheung, Ronald C M, Rezgui, Djamel, Cooper, Jonathan E

Publikováno v: Healy, F, Cheung, R C M, Rezgui, D & Cooper, J E 2021, Nonlinear Stability Analysis and Experimental Exploration of Limit Cycle Oscillations with Flared Folding Wingtips . in AIAA SCITECH 2022 Forum : Session: Flutter and Limit Cycle Oscillation Problems II . American Institute of Aeronautics and Astronautics Inc. (AIAA), 2022 AIAA SciTech Forum, San Diego, United States, 3/01/22 . https://doi.org/10.2514/6.2022-0657

Recent studies have considered the use of Flared Folding Wingtips (FFWTs) to enable higher aspect ratios - reducing overall induced drag - whilst also reducing gust loading and meeting airport operational requirements. This paper presents the first e

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8d8d8acc0e89b8877557d250628617d3
https://doi.org/10.2514/6.2022-0657

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On the Nonlinear Geometric Behaviour of Flared Folding Wingtips

Autor: Healy, Fintan, Cheung, Ronald C M, Rezgui, Djamel, Cooper, Jonathan E, Wilson, Thomas, Castrichini, Andrea

Publikováno v: Healy, F, Cheung, R C M, Rezgui, D, Cooper, J E, Wilson, T & Castrichini, A 2021, On the Nonlinear Geometric Behaviour of Flared Folding Wingtips . in AIAA SCITECH 2022 Forum : Session: Flutter and Limit Cycle Oscillation Problems II . American Institute of Aeronautics and Astronautics Inc. (AIAA), 2022 AIAA SciTech Forum, San Diego, United States, 3/01/22 . https://doi.org/10.2514/6.2022-0656

Recent studies have considered the use of flared folding wingtips (FFWTs) to enable higher aspect ratios - reducing overall induced drag - whilst reducing gust loading and meeting airport operational requirements. The majority of these analyses have

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::da2a90e174ee946a114641a2ccc24105
https://doi.org/10.2514/6.2022-0656

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Akademický článek

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Aeroelastic tailoring optimisation of a combat aircraft wing with tow-steered composites

Autor: Ali Tatar, Cheung, Ronald C. M., Cooper, Jonathan E., Pearson, David P., Clyde Warsop

Publikováno v: University of Bristol-PURE
Tatar, A, Cheung, R C M, Cooper, J E, Pearson, D P & Warsop, C 2022, ' Aeroelastic tailoring optimisation of a combat aircraft wing with tow-steered composites ', Paper presented at 19th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2022, Madrid, Spain, 13/06/22-17/06/22 .

This paper investigates the possibility of employing tailored unidirectional and fibre steered aeroelastically tailored composite lay-up techniques for a combat aircraft wing to meet performance requirements (maximise lift/drag) at more than one desi

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::a2cb58f1faccc8685fd100923709a0dc
https://research-information.bris.ac.uk/en/publications/1a76fdef-f1e5-4e30-90a6-4b6bdd91a898

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