Issue |
E3S Web Conf.
Volume 345, 2022
XXV Biennial Symposium on Measuring Techniques in Turbomachinery (MTT 2020)
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Article Number | 03001 | |
Number of page(s) | 8 | |
Section | Facilities | |
DOI | https://doi.org/10.1051/e3sconf/202234503001 | |
Published online | 29 March 2022 |
A New Test Facility for Advanced Testing of Variable Inlet Guide Vanes
1 Bundeswehr University Munich, Institute of Jet Propulsion, 85577 Neubiberg, Germany
2 MAN Energy Solutions SE, ECC Integrally Geared Compressors, 13507 Berlin, Germany
* Corresponding author: roman.frank@unibw.de
Various experimental and numerical studies of advanced blade configurations for variable inlet guide vanes (VIGVs) were conducted during the past years. Nevertheless, experimental loss characteri-zations of VIGV blade designs vastly focused on the primary profile losses. Secondary flow losses as they occur in a real engine application were often neglected. For this reason, a new wind tunnel facility was erected and commissioned at the Bundeswehr University Munich to enable extensive investigations of application-oriented annular VIGV configurations at typical low subsonic Mach numbers. Five-hole probe field traverses are established by a probe traversing unit in the in-and outflow region of the VIGV. The requirements for a further extension of the applicable measuring techniques by optical methods is moreover provided. Thus, not only profile losses caused by the blades, but also secondary flow losses generated by blade-wall flow interactions and the open blade tips can be resolved in detail.
© The Authors, published by EDP Sciences, 2022
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