@inproceedings{49b75ea0b34244d3bf4b0d7390c37010,
title = "Numerical and experimental studies of the flow field details on a cascade with end wall part-clearance",
abstract = "The paper presents numerical and experimental results for a low speed cascade with a partclearance at one endwall. The aerofoil design is representative for a variable stator vane in a modern high pressure compressor. A configuration with a gap at the rear 30% of chord and a reference cascade without endwall clearance are compared. The simulations and measurements are carried out at an inlet Mach number of Ma=0.12 and a Reynolds number of 6.6 · 105. 3D RANS simulations were performed using the Spalart Allmaras and a κ-ε turbulence model. In the experiment five-hole probe measurements were accomplished in the low speed cascade-wind tunnel at the Technische Universit{\"a}t Braunschweig to obtain the flow field data.",
author = "S. P{\"o}nick and D. Ko{\v z}ulovi{\'c} and R. Radespiel and B. Becker and V. G{\"u}mmer",
note = "Publisher Copyright: Copyright {\textcopyright} 2009 Local Organising Committee.; 8th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2009 ; Conference date: 23-03-2009 Through 27-03-2009",
year = "2009",
language = "English",
series = "8th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2009 - Conference Proceedings",
publisher = "Verlag der Technischen Universitat Graz",
pages = "317--327",
editor = "F. Heitmeir and F. Martelli and M. Manna",
booktitle = "8th European Conference on Turbomachinery",
}