% IMPORTANT: The following is UTF-8 encoded. This means that in the presence % of non-ASCII characters, it will not work with BibTeX 0.99 or older. % Instead, you should use an up-to-date BibTeX implementation like “bibtex8” or % “biber”. @PHDTHESIS{Waniczek:565874, author = {Waniczek, Phillip}, othercontributors = {Jeschke, Peter and Steffens, Klaus}, title = {{I}nstationäre {S}trömung und {B}etriebsverhalten eines mehrstufigen {T}riebwerk-{H}ochdruckverdichters beim {P}umpen}, school = {RWTH Aachen}, type = {Dissertation}, address = {Aachen}, publisher = {Shaker Verlag}, reportid = {RWTH-2016-00177}, isbn = {978-3-8440-4159-0}, series = {Berichte aus der Strömungstechnik}, pages = {VII, 165 Seiten : Illustrationen, Diagramme}, year = {2015}, note = {Druckausgabe: 2015. - Auch veröffentlicht auf dem Publikationsserver der RWTH Aachen University 2016; Dissertation, RWTH Aachen, 2015}, abstract = {In a joint research and development project between MTU Aero Engines company and the Institute of Jet Propulsion and Turbomachinery of Aachen University the unsteady flow during surge was analysed based on experimental results. For this purpose the institute developed and manufactured a new design of probe that allows a transientmeasurement of the 2-dimensional velocity vector independent of the angle of attack to the probe. For temperature measurements a fast thermocouple was integrated in the probe head for the first time. With this probe type the high dynamic process of surge was investigated in an axial compressor. The chosen compressor represents the design of modern jet engine high pressure compressors. The new probes were positioned in front and downstream of the first stage rotor of this 8-stage axial compressor. With this experimental set-up surge experiments were conducted for various speeds. In addition to the probe measurements unsteady wall pressure signals of all stages as well as blade vibration data could be included in the analysis.The experimental results provide a detailed understanding of the flow pattern in all phases of the surge cycle. This also includes the short periods of the surge cycle (flow separation and flow acceleration). In the phase of flow separation a deceleration of the flow down to axial velocities (mass flow) of zero could be shown (shut-off-point). Afterwards reverse flow starts which shows quasi-steady state conditions in terms of flow angle and Mach numbers. In this reverse flow phase the fluid enters the rotor almost perpendicular to the trailing edge. Temperature measurements show that the rotor still adds energy to the fluid. Since the compressor efficiency is very low during this phase the main portion of the energy is transferred into heat. The acceleration of the flow occurs on the basis of an abrupt static pressure difference between the rotor leading and trailing edge. The pressure difference leads to an acceleration of the flow in the axial direction and hence the flow separation vanishes. The variation of speed confirms the transition from classic surge to deep surge when speed is increased.}, cin = {413510}, ddc = {620}, cid = {$I:(DE-82)413510_20140620$}, typ = {PUB:(DE-HGF)3 / PUB:(DE-HGF)11}, urn = {urn:nbn:de:hbz:82-rwth-2016-001774}, url = {https://publications.rwth-aachen.de/record/565874}, }