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Dynamics / Turbines / Aerodynamics / Compressors / Thermodynamics / Pump / Axial compressor / Gas turbine / Fluid mechanics / Fluid dynamics / Mechanical engineering


Proceedings of the 8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows Lyon, July[removed]Paper reference : ISAIF8-008
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Document Date: 2013-09-23 15:36:24

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City

Ohlendorf / Orlando / Atlanta / Cologne / Barcelona / Montréal / Vienna / Lyon / Derby / Turner / Hills / UK In / /

Company

UK Rolls-Royce plc / EPSRC / Rolls-Royce plc / /

Country

Germany / Austria / United States / Canada / United Kingdom / Spain / /

Facility

Sussex University / University of Surrey / University of Surrey School / /

IndustryTerm

main gas path / secondary air systems / axial gas turbines / unsteady solutions / hot annulus gas / annulus gas / gas rotor-stator systems / gas ingestion / hot gas ingestion / disc cavity/main gas path modelling / main gas path flows / axial gas turbine rim seal configuration / parallel processors / /

Organization

Congress / University of Surrey School of Engineering / University of Surrey / United Nations / Sussex University / /

Person

Peter Childs / Malfa / Susanne Svensdotter / Beretta / /

Position

G.P. / P. R. N. / model / but without the TSW / reduced seal clearance model / as expected / rim seal Abbreviations TSW turbine stator well MP / Cao / MP / /

ProvinceOrState

New Jersey / A.B. / Georgia / /

PublishedMedium

The Aeronautical Journal / /

Technology

8 parallel processors / fluid dynamics / heat transfer / simulation / /

URL

http /

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