Vorticity-transport and unstructured RANS investigation of rotor-fuselage interactions
Smith, Marilyn J. and Shenoy, Rajiv and Kenyon, Adam R. and Brown, Richard (2009) Vorticity-transport and unstructured RANS investigation of rotor-fuselage interactions. In: 35th European Rotorcraft Forum, 2009-09-22 - 2009-09-25. (http://www-legacy.aero.gla.ac.uk/Research/rotorcra...)
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Abstract
The prediction capabilities of unstructured primitive-variable and vorticity-transport-based Navier-Stokes solvers have been compared for rotorcraft-fuselage interaction. Their accuracies have been assessed using the NASA Langley ROBIN series of experiments. Correlation of steady pressure on the isolated fuselage delineates the differences between the viscous and inviscid solvers. The influence of the individual blade passage, model supports, and viscous effects on the unsteady pressure loading has been studied. Smoke visualization from the ROBIN experiment has been used to determine the ability of the codes to predict the wake geometry. The two computational methods are observed to provide similar results within the context of their physical assumptions and simplifications in the test configuration.
ORCID iDs
Smith, Marilyn J., Shenoy, Rajiv, Kenyon, Adam R. and Brown, Richard ORCID: https://orcid.org/0000-0003-2754-5871;-
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Item type: Conference or Workshop Item(Paper) ID code: 27435 Dates: DateEvent22 September 2009PublishedSubjects: Technology > Mechanical engineering and machinery
Technology > Motor vehicles. Aeronautics. AstronauticsDepartment: Faculty of Engineering > Mechanical and Aerospace Engineering Depositing user: Ms Katrina May Date deposited: 13 Sep 2010 14:11 Last modified: 04 Dec 2024 01:34 URI: https://strathprints.strath.ac.uk/id/eprint/27435