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Interaction between Rotating Instability and Rotating Stall in Axial Compressors
- Interaction between rotating stall and RI disturbances
[1]
- © TUB F1
The proposed project focuses on
Rotating Instability (RI), which is known as a prestall instability in
axial compressors. Referring to own recent experimental and numerical
investigations, the physical mechanism of RI needs to be reflected on
a generic model. Based on a systematical reduction of necessary
boundary conditions, a Kelvin‐Helmholtz‐Instability is to be
generated in an annulus where the disturbances propagate
circumferentially. Afterwards pressure fluctuations being induced by
the Kelvin‐Helmholtz‐Instability will be investigated using
established analysis methods for the identification of RI.
In order to extend the scope of parameters, the impact of periodical
wakes coming from an upstream blade row onto the formation of RI will
be investigated. In detail, the main objective is to analyze the
influence of specific excitation frequencies on spectral, modal and
time‐resolved RI characteristics. In a multidisciplinary approach, a
possible influence of RI through a targeted adjustment of the number
of blades would also provide a great scientific benefit in the field
of aeroelasticity of turbomachinery. It is known that RI can be one of
the reasons for non‐synchronous blade vibrations. In addition, the
extremely short‐timed inception process of rotating stall will be
investigated under the additional influence of RI. It will be
clarified whether RI is provoking the development of stall cells and
which driving mechanisms are involved in this process.
In
this context, the interaction between RI and wellknown inception
mechanisms such as "spikes" or "modes" will be
analyzed. The results have great potential to contribute significantly
to the subject of rotating stall inception.
Over the last decades
the topic RI is part of lively but also controversial discussions.
Even the term "Rotating Instability" was considered
inappropriate by parts of the community. Thus, the proposed project
supports an unambiguous classification of RI into the field of
"compressor instabilities" and "stall
inception".
Person of contact: M.Sc. Ergin Tüzüner
[2]
Person of contact: Dipl.-Ing. (FH) Victor Bicalho [3]
Person of contact: Dr.-Ing. Mario Eck [4]
Encouraged by
the DFG, since 2020 [5]
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Contact
M.Sc. Ergin TüzünerTel. +49 (0)30 314-21320
Institute of Aeronautics & Astronautics
Room F 012
e-mail query [6]
Website [7]
Contact
Dipl.-Ing. (FH) Victor BicalhoTel. +49 (0)30 314-25008
Institute for Aeronautics & Astronautics
Room F 004
e-mail query [8]
Website [9]
Contact
Dr.-Ing. Mario EckTel. +49 (0)30 314-26919
Institute for Aeronautics & Astronautics
Room F 003
e-mail query [10]
Website [11]
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