Effects of the Inlet Flow Conditions on the Tip Clearance Flow of an Isolated Compressor Rotor
Author:
Affiliation:
1. Universita¨t der Bundeswehr Mu¨nchen, Neubiberg, Germany
2. Technische Universita¨t Braunschweig, Braunschweig, Germany
Abstract
Publisher
ASMEDC
Link
http://asmedigitalcollection.asme.org/GT/proceedings-pdf/doi/10.1115/GT2002-30639/2575087/1123_1.pdf
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Experimental analysis and modeling of the losses in the tip leakage flow of an isolated, non-rotating blade setup;Experiments in Fluids;2020-05
2. Investigations on the Effects of Inflow Condition and Tip Clearance Size to the Performance of a Compressor Rotor;Journal of Engineering for Gas Turbines and Power;2014-07-15
3. Sensitivity of Multistage Compressor Performance to Inlet Boundary Conditions;Journal of Propulsion and Power;2014-03
4. Investigation of the Shear Flow Effect on Secondary Flow and Losses in a Low Speed Axial Flow Compressor Cascade;International Journal of Gas Turbine, Propulsion and Power Systems;2014
5. Penny Gap Effect on Performance and Secondary Flowfield in a Compressor Cascade;Journal of Propulsion and Power;2012-09
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