Transonic buffet alleviation via virtual control surfaces

Petrocchi, A., Mauriello, M. and Barakos, G. (2023) Transonic buffet alleviation via virtual control surfaces. Aerospace Science and Technology, 140, 108478. (doi: 10.1016/j.ast.2023.108478)

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Abstract

In this work, computational fluid dynamics simulations are carried out to assess the ability of control surfaces to alleviate or suppress transonic buffet. Among the available control surfaces, upper trailing edge flaps were considered since they modify the aerofoil pressure distribution and fix the shock at an upstream position. Spoilers were also studied as they produce a similar effect by interfering with the pressure disturbance propagation in the boundary layer and prevent buffet. For both devices, the sensitivities to geometric parameters are studied. The effectiveness of these buffet control methods is first assessed for 2D computations around different wing sections. As spoilers were considered more effective, results on a 3D configuration are provided to discuss the influence of finite-span devices on aerodynamic performance. In addition, a simple model accounting for changes in the flight Mach number together with the spoiler is presented to simulate a simple flight scenario and provide an effective strategy for buffet suppression. In the framework of numerical investigations, the adoption of virtual control surfaces allows for avoiding difficulties associated with the modelling of slotted and deployable devices.

Item Type:Articles
Additional Information:The present work is supported by the TEAMAero European project No. 860909 - Towards Effective Flow Control and Mitigation of Shock Effects In Aeronautical Applications.
Status:Published
Refereed:Yes
Glasgow Author(s) Enlighten ID:Barakos, Professor George and Petrocchi, Mr Andrea
Authors: Petrocchi, A., Mauriello, M., and Barakos, G.
College/School:College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity
Journal Name:Aerospace Science and Technology
Publisher:Elsevier
ISSN:1270-9638
ISSN (Online):1626-3219
Published Online:26 June 2023
Copyright Holders:Copyright © 2023 The Authors
First Published:First published in Aerospace Science and Technology 140: 108478
Publisher Policy:Reproduced under a Creative Commons License

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Project CodeAward NoProject NamePrincipal InvestigatorFunder's NameFunder RefLead Dept
306721Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical ApplicationsGeorge BarakosEuropean Commission (EC)860909ENG - Autonomous Systems & Connectivity