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Institute of Turbomachinery, University of Hannover | 論文
- IGTC-19 Origin of the Vorticity of the Rotating Stall Cell of Centrifugal Compressors : Part II: Reverse Flow as Rigid Turbulent Ekman Layer Vortex Roll(Session A-7 CENTRIFUGAL COMPRESSOR II)
- IGTC-18 Origin of the Vorticity of the Rotating Stall Cell of Centrifugal Compressors : Part I: Experimental Investigation of the Nature of the Reverse Flow(Session A-7 CENTRIFUGAL COMPRESSOR II)
- IGTC-91 The Rossby Waves of Rotating Stall in Impellers : Part I: Theoretical Background of the Rossby Waves in Blade Channels(Organized Session I ROTATING STALL AND SURGE IN COMPRESSORS)
- IGTC-91 On the Mechanism of Blade Excitation due to Surge on Centrifugal Compressors(Session C-6 STRENGTH AND VIBRATION)
- IGTC-23 On the Nature of Rotating Stall in Centrifugal Compressors with Vaned Diffusers : Part II: Karman Vortices as the Controlling Mechanism(Session A-7 UNSTEADY AERODYNAMICS I)
- IGTC-22 On the Nature of Rotating Stall in Centrifugal Compressors with Vaned Diffusers : Part I: Detection of Reverse Flow(Session A-7 UNSTEADY AERODYNAMICS I)
- IGTC-79 Prediction of Blade Vibration Stress in Centrifugal Compressors due to Engine Order Excitation(Session D-4 VIBRATION II)
- IGTC-124 BLADE VIBRATION ON RADIAL IMPELLERS EXCITED BY ROTATING STALL-CELLS AND DURING SURGE(Session C-12 Vibration and Dynamics II)
- TS-14 Comparison of Flow Field and Performance of Internal and External Volutes for Centrifugal Compressors(Session A-4: Performance 1)
- TS-13 Non-Adiabatic Energy Process in Exhaust-Gas Turbines Using Heuristic Simulation Method(Session A-4: Performance 1)
- IGTC-20 Evaluation of Unsteady Blade Loading Signals during Stall and its Inception in Centrifugal Compressors(Session A-7 CENTRIFUGAL COMPRESSOR II)
- IGTC-81 Investigation of the Solidity and the Blade Vibration Behaviour of Radial Compressor Impellers due to a Significant Reduction of the Hyperbolic Undercut in the Flankmilling Process(Session D-1 VIBRATION)