Volume 16, Issue 1 pp. 421-422
Section 7
Free Access

Deformed gap space using macro-micro FEA model and transferred into a CFD model

Ali Anwar

Corresponding Author

Ali Anwar

Department of Mechanical and Aerospace Engineering, WEIR Advanced Research Centre, University of Strathclyde, Glasgow G1 1XJ, United Kingdom

phone +44 758 876 6543, fax +44 141 552 0775Search for more papers by this author
Yevgen Gorash

Yevgen Gorash

Department of Mechanical and Aerospace Engineering, WEIR Advanced Research Centre, University of Strathclyde, Glasgow G1 1XJ, United Kingdom

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William Dempster

William Dempster

Department of Mechanical and Aerospace Engineering, WEIR Advanced Research Centre, University of Strathclyde, Glasgow G1 1XJ, United Kingdom

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David Nash

David Nash

Department of Mechanical and Aerospace Engineering, WEIR Advanced Research Centre, University of Strathclyde, Glasgow G1 1XJ, United Kingdom

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First published: 25 October 2016
Citations: 1

Abstract

Using a cylindrical nozzle and seat of a Pressure Relief Valve (PRV) the surface form and waviness is modelled using actual metrological data i. e. average surface form and waviness (Wa and Wsm) in a equation image symmetry manner. To model the surface waviness the technique used is based on the summing technique created by Tsukizoe & Hisakado [1, 2] for micro contact analysis. Due to the actual surface form measurements being in the micro-meter range, the model is required to incorporate micro and macro-meter dimensions. The material in question is stainless steel. The deformed finite element analysis model is then transferred into a CAD geometry allowing the void space to be meshed and solved using computational fluid dynamics. © 2016 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim)

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