Ice accretion effects in helicopter rotor performance via multi-body and CFD approaches
Kelly, Daniel and Habashi, Wagdi G. and Quaranta, Giuseppe and Masarati, Pierangelo and Fossati, Marco (2018) Ice accretion effects in helicopter rotor performance via multi-body and CFD approaches. Journal of Aircraft, 55 (3). pp. 1165-1176. ISSN 0021-8669 (https://doi.org/10.2514/1.C033962)
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Abstract
A numerical approach for assessing the degraded aerodynamics and flight characteristics of ice-contaminated helicopter rotors is proposed. A hybrid two- and three-dimensional loose coupling strategy between Multibody Dynamics modeling and Computational Fluid Dynamics icing is formulated that attempts to balance computational resources, model complexity and accuracy for use during the early-design phases. A quasi-3D formulation that considers the heat transfer and the motion of the water film due to centrifugal effects is introduced. The method is suited for the analysis of rime, glaze and/or mixed ice conditions. Degraded aerodynamic and dynamic characteristics of the iced rotor and the changes in flight performance are assessed. The technique has been applied to the scenario of isolated helicopter rotors in hover and in forward flight. Deterioration of the figure of merit is also presented.
ORCID iDs
Kelly, Daniel, Habashi, Wagdi G., Quaranta, Giuseppe, Masarati, Pierangelo and Fossati, Marco ORCID: https://orcid.org/0000-0002-1165-5825;-
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Item type: Article ID code: 61998 Dates: DateEvent31 May 2018Published5 December 2017Published Online24 September 2017AcceptedSubjects: Technology > Motor vehicles. Aeronautics. Astronautics Department: Strategic Research Themes > Ocean, Air and Space
Faculty of Engineering > Mechanical and Aerospace EngineeringDepositing user: Pure Administrator Date deposited: 11 Oct 2017 10:58 Last modified: 11 Nov 2024 11:28 URI: https://strathprints.strath.ac.uk/id/eprint/61998