Numerical Investigation of Boundary Layers in Wet Steam Nozzles

Author:

Starzmann Jörg1,Hughes Fiona R.2,White Alexander J.1,Grübel Marius3,Vogt Damian M.3

Affiliation:

1. Hopkinson Laboratory, Department of Engineering, University of Cambridge, Cambridge CB2 1PZ, UK e-mail:

2. Whittle Laboratory, Department of Engineering, University of Cambridge, Cambridge CB2 1PZ, UK e-mail:

3. ITSM-Institute of Thermal Turbomachinery and Machinery Laboratory, University of Stuttgart, Stuttgart D-70569, Germany e-mail:

Abstract

Condensing nozzle flows have been used extensively to validate wet steam models. Many test cases are available in the literature, and in the past, a range of numerical studies have dealt with this challenging task. It is usually assumed that the nozzles provide a one- or two-dimensional flow with a fully turbulent boundary layer (BL). The present paper reviews these assumptions and investigates numerically the influence of boundary layers on dry and wet steam nozzle expansions. For the narrow nozzle of Moses and Stein, it is shown that the pressure distribution is significantly affected by the additional blockage due to the side wall boundary layer. Comparison of laminar and turbulent flow predictions for this nozzles suggests that laminar–turbulent transition only occurs after the throat. Other examples are the Binnie and Green nozzle and the Moore et al. nozzles for which it is known that sudden changes in wall curvature produce expansion and compression waves that interact with the boundary layers. The differences between two- and three-dimensional calculations for these cases and the influence of laminar and turbulent boundary layers are discussed. The present results reveal that boundary layer effects can have a considerable impact on the mean nozzle flow and thus on the validation process of condensation models. In order to verify the accuracy of turbulence modeling, a test case that is not widely known internationally is included within the present study. This experimental work is remarkable because it includes boundary layer data as well as the usual pressure measurements along the nozzle centerline. Predicted and measured boundary layer profiles are compared, and the effect of different turbulence models is discussed. Most of the numerical results are obtained with the in-house wet steam Reynolds-averaged Navier–Stokes (RANS) solver, Steamblock, but for the purpose of comparison, the commercial program ansys cfx is also used, providing a wider range of standard RANS-based turbulence models.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference36 articles.

1. The Spontaneous Condensation of Steam in Supersonic Nozzles;PhysicoChem. Hydrodyn.,1982

2. Two-Dimensional, Nonequilibrium, Wet-Steam Calculations for Nozzles and Turbine Cascades;ASME J. Turbomach.,1992

3. Št'astný, M., Šejna, M., and Jonas, O., 1997, “Modeling the Flow With Condensation and Chemical Impurity in Steam Turbine Cascade,” 2nd European Conference on Turbomachinery, pp. 81–88.

4. Numerical and Experimental Investigations of Steam Condensation in LP Part of a Large Power Turbine;ASME J. Fluids Eng.,2009

5. A Study of Spontaneous Condensation in an LP Test Turbine,2015

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