Experimental Aero Study on Turbine Rear Structures at Engine-Realistic Flow Conditions
This work summarizes the results obtained from experimental studies of the engine-realistic TRS for two design configurations: baseline (annular) and state-of-the-art (polygonal) designs equipped with OGVs of different geometries. Each of these two concepts was assembled and aerodynamically investigated for the on-design and off-design conditions in a modern 1.5 stage facility (Chalmers OGV-LPT rig) which provides realistic boundary conditions for the TRS. The aerodynamic study was performed by traverse pressure measurements for the inlet and outlet planes by multi-hole pressure probes, oil-film visualization, and static pressure measurements with embedded pressure taps. Steady state RANS simulations of the TRS were also done to estimate the prediction capabilities of a commercial CFD tool.
OGVs with increased thickness introduce slight increase of pressure losses, although the bump vane with add-on does influence the flow substantially. Apart from downstream influence with additional vorticity, generated from bump itself, and corresponding increased pressure losses, it also has upstream influence indirectly affecting inlet conditions into the TRS. For baseline configuration, the higher inlet swirl angles in the hub region result in increased vane loading and pressure losses. For state-of-the art configuration, blade- and bump-loading analysis show clear mutual influence of the bump and vane pressure distributions and, therefore, the need to design the vane and bump combination as one aerodynamic unit. Moreover, the present work gives a thorough comparison between experimental and numerical data showing that using the CFD tool captures secondary flow structures well, although CFD predictions are conservative.
Disclaimer: The content of this article reflects only the authors’ view. The Clean Sky 2 Joint Undertaking is not responsible for any use that may be made of the information it contains.
Clean Sky 2 Joint Undertaking European Union (EU) Horizon 2020 CS2-RIA EATEEM 82139
Turbine Rear Structure
Outlet Guide Vanes
Particle Image Velocimetry
Chalmers, Mekanik och maritima vetenskaper, Strömningslära
Experimental Flow Analysis in a Modern Turbine Rear Structure with 3D Polygonal Shroud Under Realistic Flow Conditions
Proceedings of European Conference on Turbomachinery Fluid dynamics,; Vol. 14(2021)
Paper i proceeding
Detailed Experimental Study of the Flow in a Turbine Rear Structure at Engine-Realistic Flow Conditions
Journal of Turbomachinery,; Vol. 143(2021)
Artikel i vetenskaplig tidskrift
Experimental and numerical flow analysis of an engine-realistic state-of-the-art turbine rear structure
Proceedings of the ASME Turbo Expo 2021 Virtual Conference and Exhibition,; Vol. 2B-2021(2021)
Paper i proceeding
AT3E - Aerotermoutveckling för effektiva jetmotorutlopp
VINNOVA (2017-04861), 2017-11-10 -- 2022-06-30.
Experimentell aerotermisk studie av nästa generations flygmotorkomponenter
Europeiska kommissionen (EU) (EC/H2020/821398), 2018-10-01 -- 2021-03-31.
Rymd- och flygteknik
Strömningsmekanik och akustik
Navier Room, Hörsalsvägen 7A, Chalmers
Opponent: Zuher Abdel Mallak, GKN Aerospace Sweden AB