A new linear high speed compressor stator cascade for active flow control investigations
C Tiedemann, A Heinrich, D Peitsch - 6th AIAA Flow Control …, 2012 - arc.aiaa.org
C Tiedemann, A Heinrich, D Peitsch
6th AIAA Flow Control Conference, 2012•arc.aiaa.org… First active flow control investigations are presented in this paper. A variation of the
incidence and the inflow Mach number as well as variations of the jets mass … At the
Institute of Aeronautics and Astronautics of TU Berlin a linear stator cascade test rig
equipped with highly loaded compressor stators was installed to examine Active Flow
Control methods for the compressible Mach number range. First investigations of the base
flow and steady and pulsed injected flow actuation are presented in this work. …
incidence and the inflow Mach number as well as variations of the jets mass … At the
Institute of Aeronautics and Astronautics of TU Berlin a linear stator cascade test rig
equipped with highly loaded compressor stators was installed to examine Active Flow
Control methods for the compressible Mach number range. First investigations of the base
flow and steady and pulsed injected flow actuation are presented in this work. …
Aircraft manufacturers and airlines demand for highly efficient engines to address the more and more stringent requirements in terms of economy and environmental compatibility. This target requires light and
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